The Online Books Page

Online Books by

Arnold Engineering Development Center

Books from the extended shelves:

• Arnold Engineering Development Center: 0.2-scale B-1 external-compression inlet verification model test at transonic and supersonic Mach numbers : phase II (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by R. C. German, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Ablation and viscous effects on the force and moment characteristics of slender cone models at Mach 10 under laminar flow conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by B. J. Griffith, B. M. Majors, W. T. Strike, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: AEDC high alpha aerodynamics. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by Inc ARO and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: AEDC test facilities handbook. (Arnold Engineering Development Center, Air Force, 1959) (page images at HathiTrust)
• Arnold Engineering Development Center: The AEDC three-dimensional, potential flow computer program. Volume I. Method and computer program (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Donald C. Todd, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: The AEDC three-dimensional, potential flow computer program. Volume II. Mathematical modeling, application, and verification (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Richard L. Palko, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic and cold jet plume geometry characteristics of the Army free rocket at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by E. S. Washington, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic calibration and shakedwon testing of the full-scale F-15 aircraft inlet simulator (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by W. F. Kinzey, E. S. Gall, V. O Williams, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics and store loads of a 1/24-scale F-111 aircraft model with three external store loadings (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by C. F. Anderson and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of a full-scale F-101 ejection seat with an anthropomorphic dummy at free-stream Mach numbers from 0.2 to 0.8 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Lawrence L. Galigher, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of an ejection seat escape system with a stabilization parachute at Mach numbers from 0.3 through 1.2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by David E. A. Reichenau, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of low aspect ratio fins at Mach numbers from 0.80 to 1.30 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by D.K. Smith, R. C. German, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of perforated walls for transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. L. Jacocks, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. M. Whoric, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of the B-1 fuselage afterbody including simulated jet exhaust effects at Mach numbers from 0.55 to 2.20 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973, 1973), also by Earl A. Price, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. H. Jones, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic interference effects on various weapon shapes in the flow field of a transonic wing configuration at Mach numbers from 0.5 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by G. R. Mattasits, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aerodynamic loads data on the M-117 bomb in the flow field of the triple ejection rack at Mach numbers from 0.5 to 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Willard E. Summers, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: The AFFDL-Nielsen flow-field study (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by William T Strike, John H. Porter, Terry R. Penney, Nielsen Engineering & Research, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Afterbody drag investigation of a twin-nozzle fighter-type model at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by Earl A. Price, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Aircraft motion sensitivity to cross and cross-coupling damping derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. W. Butler, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Aircraft motion sensitivity to dynamic stability derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. F. Langham, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Altitude-velocity table and charts for imperfect air. Volume I. Free-stream stagnation gas composition data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Clark H. Lewis, E. G. Burgess, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: An analysis of initial static pressure probe measurements in a low-density hypervelocity wind tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by David E. Boylan, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analysis of laminar boundary layers on right circular cones at angle of attack, including streamline-swallowing effects (Arnold Air Force Station, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, 1972., 1972), also by Arloe Wesley Mayne and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Analysis of the measured effects of the principal exhaust effluents from solid rocket motors (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), also by R. Dawbarn, D. J. Watson, Max Kinslow, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Arnold Engineering Development Center: Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by John C. Adams, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analysis of three-dimensional inviscid supersonic flow between a body and an outer wall : with application to a jet stretcher system (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by W. C. Armstrong, R. C. Bauer, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Steven F. Yaros, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: An analytic investigation of accuracy requirements for onboard instrumentation and film data for dynamically scaled wind tunnel drop models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1997., 1997), also by K. S. Keen, R. L. Arterbury, C. H. Morgret, Inc Sverdrup Technology, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical and experimental thermal analysis of a guided bomb (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by W. K. Crain, R. K. Matthews, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. W. Swafford, R. K. Matthews, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical description of the complete two-dimensional turbulent boundary-layer velocity profile (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by David L. Whitfield, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical nodel of supersonic, turbulent, near-wake flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical, numerical, and experimental results on turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by David L. Whitfield, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An analytical study of hypersonic inlets in free-molecule flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Max Kinslow, M. R. Busby, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An Analytical study of the use of air-equivalent hot gaseous mixtures for aerodynamic test purposes (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by Kenneth E. Tempelmeyer, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Analytical study of ventilated wind tunnel boundary interference on V/STOL models including wake curvature and decay effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by E. M. Kraft, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Application of linearized transonic theory to tunnel blockage interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), also by C. F. Lo, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Application of splines to the numerical solution of two-point boundary-value problems (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Donald C. Todd, John C Adams, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An application of the Chapman-Korst theory to supersonic nozzle-afterbody flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by R. C. Bauer, J. H. Fox, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Application of the vortex-lattice method to represent a jet exhausting from a flat plate into a crossflowing stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by F. L. Heltsley, R. L. Parker, Martin Marietta Corporation, McDonnell Douglas Corporation, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Applications of the aerotherm BLIMP boundary-layer program to nonablating reentry flight conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by Emmett E. Edenfield, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: An approximate analysis of the shock structure in underexpanded plumes (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Arnold Engineering Development Center high-temperature testing capabilities (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. H. Trimble, R. K. Matthews, R. T. Smith, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Artificially induced boundary-layer transition on blunt-slender cones using distributed roughness and spherical-type tripping devices at hypersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by A. H. Boudreau, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Blockage study of a 1/16-scale B-1 inlet model in the 1-ft transonic and supersonic tunnels of the Propulsion Wind Tunnel Facility (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by C. F. Anderson, F. M. Jackson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Boundary-layer characteristics at Mach numbers 2 through 5 in the test section of the 12-inch supersonic tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by D. R. Bell, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Boundary-layer transition correlation on a slender cone in wind tunnels and flight for indications of flow quality (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by N. Sam Dougherty, David F. Fisher, Hugh L. Dryden Flight Research Center, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Boundary-layer transition on cones near Mach one in an aeroballistic range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. Leith Potter, J. R. Myers, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Boundary-layer transition under hypersonic conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. Leith Potter, Jack D. Whitfield, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Calculation of interference for a porous wall wind tunnel by the method of block cyclic reduction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by C. F. Lo, H. N. Glassman, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Calculation of skin friction intwo-dimensional, transonic, turbulent flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by T. W. Swafford, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Calculation of the boundary-layer flow in the windward symmetry plane of a spherically blunted axisymmetric body at angle of attack, including streamline-swallowing effects (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Arloe W. Mayne, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Calculation of the boundary-layer growth in a Ludwieg tube (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by James C. Sivells, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Calibration and performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by W. T. Strike, Calspan Field Services, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by F. M. Jackson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion test section at various Reynolds numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by F. M. Jackson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Calibration tests of a Litton conical air data probe at Mach numbers of 2 to 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by Scott R. Mallard, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Captive aircraft testing at high angles of attack (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by R. W. Butler, J. P. Christopher, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Captive trajectory system for AEDC supersonic wind tunnel (A) and hypersonic wind tunnels (B) and (C) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by T. D. Buchanan, W. A. Crosby, United States. Air Force. Arnold Air Force Base, and Calspan Field Services (page images at HathiTrust)
• Arnold Engineering Development Center: CFD wing/pylon/finned store mutual interference wind tunnel experiment (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by E. Rolland Heim and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Characteristic boundary conditions for ARO-1 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by Karl R. Kneile, James L. Jacocks, Donald C. Todd, Calspan Field Services, Inc Sverdrup Technology, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Characteristics of axisymmetric and two-dimensional isoenergetic jet mixing zones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by R. C. Bauer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Chemical kinetic regimes of hypersonic flight simulation (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by Donald J. Harney and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Chimera : a grid-embedding technique (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1986., 1986), also by J. A. Benek, F. C. Dougherty, J. L. Steger, Ames Research Center, Calspan Corporation, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Cluster formation in free-jet expansions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by A. B. Bailey, R. Dawbarn, M. R. Busby, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Combined effects of viscous interaction and ideal source flow on pressure and heat-transfer distributions over hemisphere cylinders at M infinity is approximately 18 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. H. Eaves, Clark H. Lewis, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Comments on the use of measurements of the effective moment parameter (C m alpha) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by C. J. Welsh, Calspan Field Services, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Common geometry systems for the numerical representation of three-dimensional aerodynamic configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1984., 1984), also by K. Scott Keen, United States. Air Force. Arnold Air Force Base, and Calspan Field Services (page images at HathiTrust)
• Arnold Engineering Development Center: Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. E. Edenfield, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Comparison of store trajectory and aerodynamic loads, and model flow-field characteristics obtained in the AEDC PWT/4T and VFK/A wind tunnels at Mach number 1.63 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. W Hill, R. H. Tolbert, J. T. Best, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by C. J. Schueler, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Comparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Comparison of wind tunnel and flight test measurements of static aerodynamic loading of a captive store (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. E. Dix, G. R. Mattasits, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Comparisons of free-flight and wind tunnel data on slender cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by B. J. Griffith, Leo G. Siler, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume III. Appendixes F, Test number 6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Inc ARO, Air Force Armament Laboratory (U.S.), and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: A compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume I (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Air Force Armament Laboratory (U.S.), Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume II. Appendixes A through E, Test numbers 1 through 5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Inc ARO, Air Force Armament Laboratory (U.S.), and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Computation of axisymmetric separated nozzle-afterbody flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by James L. Jacocks, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A computer study of hypersonic laminar boundary-layer/shock-wave interaction using the time-dependent compressible Navier-Stokes equations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Darman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by B. K. Hodge, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Corrections to single-shielded total temperature probes in subsonic, supersonic, and hypersonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by M. O. Varner, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: A Correlation of artifically induced boundary-layer transition data from blunt slender cones at hypersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by A. H. Boudreau, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Correlation of experimental and theoretical steady-state spinning motion for a current fighter airplane using rotation-balance aerodynamic data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by T. F. Langham, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Critical sting length as determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at Mach number 3 for reduced frequencies of 0.0033 and 0.0056 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynaqmics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by Bob L. Uselton, Fred B. Cyran, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Database for internal store carriage and jettison (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by R. E. Dix, T. W. Dobson, Air Force Armament Laboratory (U.S.), and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Database for internal store carriage and jettison. Volume II, Appendix A, configuration/run number index to the WICS database (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1990., 1990), also by R. E. Dix, T. W. Dobson, Calspan Corporation, Air Force Armament Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Development of design criteria, cost estimates, and schedules for an MHD high performance demonstration experiment; final report. (U. S. Dept. of the Interior, Office of Coal Research], 1973) (page images at HathiTrust)
• Arnold Engineering Development Center: Documentation of a transonic wind tunnel test to investigate the separation characteriscis of the GBU-10C/B, the CBU-58, and the BL-755 stores from the F-16 aircraft (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by J. M. Wright, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Documentation of the Phase III 0.192-scale Northrop/McDonnell-Douglas F-18 inlet performance test at mach numbers 0 to 1.55 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by Jimmy Walker, Sverdrup Corporation, and United States. Naval Air Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels : theory and application (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Samuel R. Pate, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Dynamic stability characteristics of a 10-deg cone at Mach number 20 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. H. Urban, R. J. Shanahan, Inc ARO, and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: Dynamic stability characteristics of a10-deg cone at Mach number 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by A. E. Hodapp, G. E. Burt, B. L. Uselton, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: The effect of plenum volume on the test section flow characteristics of a perforated wall transonic tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by C. F. Anderson, O. P. Credle, A. Anderson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: The effect of pressure pulsations and vibrations on fully developed pipe flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Donald O. Barnett, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by L. G. Siler, H. E. Deskins, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Effects of acoustic and vortical disturbances on the turbulent boundary layer at free-stream Mach number 0.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by John A. Benek, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Effects of mass transfer into laminar and turbulent boundary layers over cones at angle of attack (Blacksburg, Virginia : Virginia Polytechnic Institute and State University, 1975., 1975), also by Michael C. Frieders and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Arnold Engineering Development Center: Effects of unit Reynolds number, nose bluntness, and roughness on boundary layer transition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), also by J. Leith Potter, Jack D. Whitfield, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Effects of wall cooling and leading-edge blunting on ramp-induced, laminar flow separations at Mach numbers from 3 through 6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. Don Gray, G. L. Winchenbach, R. W. Rhudy, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An empirical look at tolerances in setting icing test conditions with particular application to icing similitude (:, 1988), also by C. S. Bartlett, Federal Aviation Administration Technical Center (U.S.), and Inc Sverdrup Technology (page images at HathiTrust)
• Arnold Engineering Development Center: Engineering model of unsteady flow in a cavity (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by R. C. Bauer, R. E. Dix, Calspan Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Equations and charts for the evaluation of the hypersonic aerodynamic characteristics of lifting configurations by the Newtonian theory (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. L. Clark, L. L. Trimmer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Equations for store separation motion simulations and instrumented model data reduction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1996., 1996), also by K. S. Keen, Calspan Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of a method for computation of separated, turbulent, compressible boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by M. C. Altstatt, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of an internal balance-supporting bracket simulating lug suspension for captive stores in wind tunnel tests (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by L. L. Galigher, R. C. Bauer, Steven F. Yaros, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of critical sting length on a 7-deg cone as determined by measurements of dynamic stability derivatives and base pressure for Mach numbers 0.2 through 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Frederick B. Cyran, Edward J. Marquart, Bob L. Uselton, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by William Lee Peters, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An Evaluation of nozzle afterbody code : ARO2P (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1986., 1986), also by Frederick C. Guyton, United States. Air Force. Arnold Air Force Base, and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of Reynolds number and tunnel wall porosity effects on nozzle afterbody drag at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by C. E. Robinson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of the aerodynamic interference of the tunnel 4T Captive Trajectory System on the separation characteristics of the BLU-27 store (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Wallace Luchuk, David W Hill, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by Lawrence L. Galigher, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by C. E. Robinson, M. Dean High, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by C. E. Robinson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Expansion of a jet into near vacuum (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Aerospace Environmental Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. A. Cassanova, W. B. Stephenson, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: An experimental and analytic investigation of a transonic shock-wave/boundary-layer interaction (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by M. C. Alstatatt, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental and theoretical study of cavity acoustics (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 2000., 2000), also by R. E. Dix, R. C. Bauer, Inc Sverdrup Technology, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by David E. Boylan, William H. Sims, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. Leith Potter, John T. Miller, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An experimental investigation of ducted, reactive, turbulent jet mixing with recirculation. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by D. E. Chriss, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An Experimental investigation of techniques to suppress edgetones from perforated wind tunnel walls (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by N. Sam. Dougherty and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental investigation of the effect of various scaling laws on the quality of the free-drop store separation simulation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. A. Paulk, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental Magnus and static stability characteristics of ballistic projectiles with various boattail angles and lengths at Mach numbers from 0.5 through 2.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnell Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by Leroy M. Jenke, T. O. Shadow, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Experimental method for correcting nozzle afterbody drag for the effects of jet temperature (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by W. L. Peters, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An Experimental study of several wind tunnel wall configurations using two V/STOL model configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by T. W. Binion, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An Experimental study of sharp and blunt 6 degree cones at large incidence with a turbulent boundary layer at Mach 6 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, High Speed Aero Performance Branch, Flight Mechanics Division, Air Force Systems Command, United States Air Force, 1974., 1974), also by E. D. McElderry, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. F. Starr, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Flow characteristics of a 12-in. intermittent supersonic tunnel (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. Anderson, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Flow-field characteristics and aerodynamic loads on external stores near the fuselage and wing-pylon positions of a swept-wing/fuselage model at Mach numbers of 0.4 and 0.7: phase V (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by R. H. Roberts, J. R. Myers, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Flow-field study about a hemisphere-cylinder in the transonic and low supersonic Mach number range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by T. Hsieh, B. M. Majors, W. T. Strike, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Flow generation properties of five transonic wind tunnel test section wall configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. L. Parker and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Flow phenomena in starting a hypersonic shock tunnel (Buffalo, New York : Cornell Aeronautical Laboratory, 1955., 1955), also by Herbert S. Glick, William E. Smith, Abraham Hertzberg, United States. Air Force. Air Research and Development Command, and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Arnold Engineering Development Center: Flow visualization photographs of a yawed tangent ogive cylinder at Mach number 2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. H. Jones, J. E. O'Hare, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Flow visualization techniques for use in hypersonic wind tunnels (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. W. Rhudy, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Force and pressure tests of an AGARD Calibration Model B at a Mach number of 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by R. K. Matthews, L. L Trimmer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Force and pressure tests of two elliptic ogive body shapes at Mach numbers 5, 6, and 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), also by Jack L. Burk, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Force and pressure tests on cones with simulated ablated noses at Mach numbers 8 and 16 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by J. S. Hahn, H. R. Little, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Force measurements on a data capsule in the wake and flow field of a carrier vehicle at Mach 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by L. D. Kayser, G. H. Merz, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Force tests of standard hypervelocity ballistic models HB-1 and HB-2 at Mach 1.5 to 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by J. Don Gray, E. Earl Lindsay, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Forces and moments on base cover plates in the wake of a discoverer Mark 4 re-entry vehicle at transonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), also by H. L. Chevalier, P. D. Gerke, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Free-flight investigation of ablation effects n the stability of conical reentry configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by C. J. Welsh, G. L. Winchenbach, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Free turbulent mixing : a critical evaluation of theory and experiment (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Philip Thomas Harsha, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Fundamental studies of subsonic and transonic flow separation. Part I. First phase summary report (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by Zhengming Wu, K. Anjaneyulu, Herbert Venghaus, L. Shen, R. Nygaard, C. H. Chen, K. C. Reddy, G. M. Elfstrom, Trevor H. Moulden, University of Tennessee (System). Space Institute, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Fundamental studies of subsonic and transonic flow separation. Part II. Second phase summary report (Tullahoma, Tennessee : University of Tennessee Space Institute, 1977., 1977), also by Zhengming Wu and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Arnold Engineering Development Center: Fundamental studies of subsonic and transonic flow separation. Part III. Third phase summary report (Tullahoma, Tennessee : The University of Tennesse Space Institute, Gas Dynamics Division, 1979., 1979), also by Zhengming Wu and University of Tennessee (System). Space Institute (page images at HathiTrust)
• Arnold Engineering Development Center: Further experiments on impact-pressure probes in a low-density, hypervelocity flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by A. B. Bailey, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Generalized base-flow analysis with initial boundary-layer and chemistry effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John H. Fox, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Heat-transfer and flow-field tests of the McDonnell Douglas-Martin Marietta space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by R. K. Matthews, R. H. Eaves, W. R. Martindale, Martin Marietta Corporation, McDonnell Douglas Corporation, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Heat-transfer and flow-field tests of the North American Rockwell/ General Dynamics Convair space shuttle configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by W. R. Martindale, L. L. Trimmer, R. K. Matthews, North American Rockwell Corporation, General Dynamics Corporation. Convair Division, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by M. E. Hillsamer, J. P. Rhudy, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Holographic interferometry measurements of subsonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. W. Sinclair, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Hydrology and tree distribution patterns of karst wetlands at Arnold Engineering Development Center, Tennessee (U.S. Dept. of the Interior, U.S. Geological Survey ;, 1996), also by William J. Wolfe and Geological Survey (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: Hypersonic force, pressure, and heat transfer investigations of sharp and blunt slender cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by David B. Wilkinson, Shelby A. Harrington, Cornell Aeronautical Laboratory, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Hypersonic lifting body windward surface flow-field analysis for high angles of incidence (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by John C. Adams, William R. Martindale, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An Improved interaction method for calculating exhaust nozzle boattail flows (Mountain View, California : Nielsen Engineering & Research, Inc., 1980., 1980), also by Gary D. Kuhn, United States. Air Force. Arnold Air Force Base, and Nielsen Engineering & Research (page images at HathiTrust)
• Arnold Engineering Development Center: The Inertial impaction of small particles (Columbus, Ohio : Battelle Memorial Institute, 1958., 1958), also by M. N. Golovin, A. A. Putnam, United States. Air Force. Air Research and Development Command, and Battelle Memorial Institute (page images at HathiTrust)
• Arnold Engineering Development Center: The influence of slight leading-edge bluntness on boundary-layer transition at a Mach number of eight (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by Jack D. Whitfield, J. Leith Potter, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An influence of the orifice on measured pressures in rarefied flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by J. Leith Potter, David E. Boylan, Max Kinslow, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5. Volume I, Experimental methods and summary of results (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by N. Sam Dougherty, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Influence of wind tunnel noise on the location of boundary-layer transition on a slender cone at Mach numbers from 0.2 to 5.5. Volume II, Tabulated and plotted data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by N. Sam Dougherty, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Influences of sting support on aerodynamic loads acting on captive store models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. E. Dix, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Influences of sway braces and mounting gaps on the static aerodynamic loading of external stores (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by R. E. Dix, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Injection of particles through a jet nozzle laterally into a supersonic airstream (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by E. E. Hilliard, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Inlet performance characteristics of a 1/5 scale Northrop YF-17 model at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by M. E. Sanders, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Inlet performance characteristics of a generalized 1/4-scale tactical aircraft models at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1971., 1971), also by R. F. Lauer, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Inlet performance characteristics of a generalized 1/5.2-scale aircraft model at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Jimmy Walker, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Integral analysis of ducted two-stream mixing with recirculation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An integral equation method for boundary interference in a perforated-wall wind tunnel at transonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by E. M. Kraft, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Integral solution of compressible turbulent boundary layers using improved velocity profiles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by David L. Whitfield, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Interactions produced by sonic lateral jets located on surface in a supersonic stream (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by W. T. Strike, J. S. Deitering, C. J. Schueler, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Interference on a model afterbody from downstream support hardware at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Earl A. Price, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by A. V. Spratley, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of an upper stage rocket plane with external-burning thrust augmentation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by E. E. Callens, J. Leith Potter, J. T. Miller, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1961., 1961), also by W. T. Strike, S. Pate, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of boundary-layer transition on swept wings at mach numbers 2.5 to 5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by S. R. Pate, R. E. Brillhart, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by S. R. Pate, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of drag reduction by boundary-layer suction on a body of revolution at Mach numbers 2.5, 3, and 3.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Research and Development Command, United States Air Force, 1965., 1965), also by S. R. Pate, Inc ARO, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of drag reduction by boundary-layer suction on a flat plate and a 36-deg swept wing at supersonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by S. R. Pate, J. S. Deitering, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of ducted, two-stream, variable-density, turbulent jet mixing with recirculation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by Roy J. Schulz, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by Earl A. Price, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of flow separation on a two-dimensional flat plate haveing a variable-san trailing-edge flap at M [free stream] = 3 and 5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by S. R. Pate, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of separated flow about a hemisphere-cylinder at 0- to 19-deg incidence in the Mach number range from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by T. Hsieh, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. L. Baer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Travis W. Binion, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of sting interference effects on an oscillating cone in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Frederick B. Cyran, J. P. Christopher, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of subsonic annular nozzles for engine exhaust/external flow interaction studies (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by R. J. Matz, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of suction controlled boundary layer on a Northrop model at Mach numbers of 2, 5, 3, and 3.5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by W. T. Strike, J. C. Donaldson, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Investigation of the effects of nose bluntness on natural and induced boundary-layer transition on axisymmetric bodies in supersonic flow (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Jack D. Coats, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: An Investigation of the effects of nose geometry on the aerodynamic characteristics of a full scale vertical launch ASROC forebody at M₀₀ = 0.30 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1987., 1987), also by R. M. Vaeth, Calspan Corporation, and Naval Ocean Systems Center (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of the effects of shock impingement on a blunt leading edge (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by A. D. Ray, R. L. Palko, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: An Investigation of the equilibrium pressure along unequally heated tubes (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by G. D. Arney, A. B. Bailey, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by T. O. Shadow, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: An Investigation of three-dimensional wall interference in a variable porosity transonice wind tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), also by Travis W. Binion, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Inviscid and viscous hypersonic nozzle flow with finite rate chemical reactions (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by E. S. Levinsky, Jerome James Brainerd, General Dynamics Corporation. Astronautics Division, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Inviscid blunt leading effects on planar surface pressure distributions at Mach number 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by W. T. Strike, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Jet simulation techniques : simulation of temperature effects by altering gas composition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. L. Peters, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. Don Gray, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by David E. Boylan, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Laser-Raman flow-field diagnostics of two large hypersonic test facilities (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. D. Williams, L. L. Price, H. M. Powell, D. A. Wagner, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Longitudinal force charactristics of two AFFDL MDF-4 high lift-to-drag configurations at Mach number 19 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by A. R. Wallace, L. G. Siler, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Longitudinal static stability and inlet drag characteristics of the McDonnell Douglas F-15 tactical fighter aircraft at Mach numbers of 1.60 and 2.20 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1971., 1971), also by F. J. Keeney, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Low-density boundary-layer modulation by suction in a hypersonic nozzle (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by Max Kinslow, J. Leith Potter, M. R. Busby, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Low-density hypervelocity wind tunnel diffuser performance (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by M. W. Milligan, J. F. Bailey, Knoxville. Department of Mechanical and Aerospace Engineering niversity of Tennessee, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A magnetic-guideway/guided-projectile system concept for aeroballistic ranges (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by George D Arney, Charles W Pender, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Magnetic suspension of wind tunnel models (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by P. L. Clemens, A. H. Cortner, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Measurement of the pressure fluctuations in the test section of the 1-foot transonic tunnel in the frequency range from 5 to 1250 cps (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. E. Robertson, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Measurement of the pressure flucuations in the test section of the 16-foot transonic circuit in the frequency range from 5 to 1000 CPS (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), also by H. L. Chevalier, H. E. Todd, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: A mehod for the prediction of the effects of free-stream disturbances on boundary-layer transition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. A. Benek, M. Dean High, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Method for calculation of the one-dimensional nonequilibrium flow of a general gas mixture through a hypersonic nozzle (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by George Emanuel, Walter G. Vincenti, Stanford University. Department of Aeronautics and Astronautics, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Method for computing boundary-layer flows, including normal pressure gradient and longitudinal curvature effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by Arloe W. Mayne, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: A method for estimating jet entrainment effects on nozzle-afterbody drag (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. C. Bauer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Method of calculating turbulent-boundary-layer growth at hypersonic Mach numbers (Arnold Air Force Base, Tennessee, Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by James C. Sivells, Robert G. Payne, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: A method of characteristics computer program for three-dimensional supersonic internal flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by W. C. Armstrong, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Methods of approximating inviscid jet boundaries for highly underexpanded supersonic nozzles (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by J. R. Henson, J. E. Robertson, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: MHD high performance demonstration experiment (Dept. of Energy ;, 1978), also by United States. Department of Energy (page images at HathiTrust)
• Arnold Engineering Development Center: Missile motion sensitivity to dynamic stability derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. F. Langham, E. S. Washington, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel (Arnold Air Force Base, Tennessee : Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by J. E. Robertson, Wyle Laboratories, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Modifications to MacCormack's 2-D Navier-Stokes compression ramp code for application to flows with axes of symmetry and wall mass transfer (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by Richard G. Hindman, Edward J. Marquart, Bob L. Uselton, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Nacelle afterbody drag investigation of a B-1 0.06-scale model at Mach numbers from 0.55 to 2.2 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by M. L. Homan, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: NEQPAK, the AEDC thermochemical nonequilibrium package : theory and use (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1994., 1994), also by J. T. Curtis, R. W. Tramel, Calspan Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Noise generation in transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by M. O. Varner, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Numerical analysis of recirculating ducted flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by R. J. Schulz, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Numerical analysis of turbulent separated subsonic diffuser flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. C. Chien, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil (Arnold Air Force Base, Tennessee : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by John C. Adams, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Numerical computation of subsonic conical diffuser flows with nonuniform turbulent inlet conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by J. C. Chien, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Numerical stability analysis of a compressor model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by K. C. Reddy, Yeng-Yung Tsui, University of Tennessee (System). Space Institute, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A Parametric investigation of the annular jet concept for obtaining afterbody drag data at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Earl A. Price, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: PARC code : theory and usage (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by G. K. Cooper, J. R. Sirbaugh, Inc Sverdrup Technology, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: PARC code validation for propulsion flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1989., 1989), also by G. K. Cooper, W. J. Phares, G. D. Garrard, United States. Air Force. Arnold Air Force Base, and Inc Sverdrup Technology (page images at HathiTrust)
• Arnold Engineering Development Center: PEGSUS 4.0 User's Manual (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1991., 1991), also by N. E. Suhs, R. W. Tramel, Calspan Corporation, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by O. P. Credle, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), also by W. N. MacDermott, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Pressure and static force test of three elliptic missile body configurations at mach numbers 1.5 to 5.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by M. E. Sellers, L Siler, Air Force Wright Aeronautical Laboratories, and Calspan Field Services (page images at HathiTrust)
• Arnold Engineering Development Center: Pressure distribution and flow visualization tests of a 1.5 elliptic cone at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by R. L. Palko, A. D. Ray, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Pressure distribution tests of several sharp leading edge wings, bodies, and body-wing combinations at Mach 5 and 8 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), also by R. E. Randall, J. L. Burk, D. R. Bell, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Pressure test of three elliptic missile body configuratins (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1985., 1985), also by Marvin E. Sellers and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Pressure tests on the standard hypervelocity ballistic model HB-2 at Mach 1.5 to 5 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by Jerry H. Jones, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Problems underlying the numerical integration of the chemical and vibrational rate equations in a near-equilibrium flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by George Emanuel, Stanford University. Department of Aeronautics and Astronautics, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds (Wright-Patterson Air Force Base, Ohio : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by J. A. Durand, J. P. Rhudy, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Real-gas effects on the aerodynamics of blunt cones as measured in a hypervelocity range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by C. J. Welsh, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Real-gas laminar boundary layers in hypervelocity nozzles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Willard E. Summers, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Real gas scale effects on hypersonic laminar boundary-layer parameters including effects of entropy-layer swallowing (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. C. Adams, E. O. Marchand, A. W. Mayne, W. R. Martindale, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Research on adaptive wall wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by Robert J. Vidal, J. C Erickson, United States. Air Force. Systems Command, and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Results of 0.2-scale B-1 production inlet development and verification tests at subsonic and supersonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. F. Lauer, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Results of a 0.1-scale B-1 inlet model test at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by F. J. Graham, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Results of a 0.2-scale B-1 inlet verification model test at transonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by John F. Riddell, F. M. Jackson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Results of a full-scale B-1 inlet/engine compatibility test at subsonic and supersonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by H. E. McDill, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Results of the full-scale F-15 inlet/engine compatibility test at subsonic and supersonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1972., 1972), also by H. E. McDill, J. L. Jacocks, R. F. Lauer, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Roll-damping derivative calculations for spinning sharp and blunt cones in supersonic and hypersonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by Arloe W. Mayne, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies. Part I, Detailed surface measurements (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John A. Benek, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies. Part II. Detailed flow measurements (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John A. Benek, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Shock-fitting for full potential equation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. M. Hafez, Earll M. Murman, United States. Air Force. Systems Command, and inc Flow Research (page images at HathiTrust)
• Arnold Engineering Development Center: The shock shape and shock detachment distance for spheres and flat-faced bodies in low-density, hypervelocity, argon flow (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by A. B. Bailey, W. H. Sims, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Simplified input for certain aerodynamic nose configurations to the Grumman QUICK-geometry system : a KWIKNOSE User's Manual (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Frederick L. Shope, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Skin-friction measurements at subsonic and transonic Mach numbers with embedded-wire gages (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by D. W. Sinclair, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Skin friction measurements at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by Charles L. Smith and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Solution for the transient one-dimensional heat conduction in an infinite slab (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by John T. Miller, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Sound and pressure measurements in cavities on a body of revolution at supersonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), also by J. C. Donaldson, D. R. Bell, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Static aerodynamic characteristics of a series of generalized slender bodies with and without fins at Mach numbers form 0.6 to 3.0 and angles of attack from 0 to 180 deg. Volume 1 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by William B. Baker, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Static force and moment test of the Holloman narrow-gage rocket slet at Mach numbers from 3.5 to 5.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1987., 1987), also by C. L. Ratliff and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Static force and moment tests of the Holloman narrow-gage rocket sled at Mach Numbers from 1.5 to 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. H. Rhudy, J. D. Corce, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Static force tests at Mach 8 of sharp and blunt 20-deg half-angle cones with a blunt 70-deg swept delta wing (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1962., 1962), also by G. H. Merz, O. R. Pritts, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Static pressure on sharp and blunt cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by Max Kinslow, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Static stability and drag characteristics of a hypersonic aircraft design at Mach numbers 1.5 to 5.6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. T. Jr Best, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1974., 1974), also by J. T. Best, R. W. Rhudy, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Static stability test of three elliptic missile body configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1985., 1985), also by Marvin E. Sellers and Calspan Corporation (page images at HathiTrust)
• Arnold Engineering Development Center: Sting dynamics of wind tunnel models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by James P. Billingsley, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by Bob L. Uselton, Frederick B. Cyran, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Sting interference effects on the Modified Basic Finner Missile at Mach numbers 0.3 through 1.3 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by Edward J. Marquart, Calspan Field Services, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Store separation testing techniques at the Arnold Engineering Development Center. Volume I, An overview (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. B. Carman, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Store separation testing techniques at the Arnold Engineering Development Center. Volume II, Description of captive trajectory store separation testing in the aerodynamic wind tunnel (4T) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. B. Carman, J. P. Christopher, D. W. Hill, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Store separation testing techniques at the Arnold Engineering Development Center. Volume III, Description and validation of Captive trajectory store separation testing in the Von Karman Facility. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by J. P. Billingsley, J. T. Best, R. H. Burt, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Store separation testing techniques at the Arnold Engineering Development Center. Volume IV, Description of dynamic drop store separation testing (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by E. G Allee, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Studies of the exhaust products from solid propellant rocket motors (Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, 1976), also by R Dawbarn, Max Kinslow, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Arnold Engineering Development Center: A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by N. Sam Dougherty, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by B. J. Griffith, Clark H. Lewis, and Inc. AEDC Division Sverdrup/ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Summary report on aerodynamic characteristics of standard models HB-1 and HB-2 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), also by J. Don Gray, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: A superconducting magnet dewar missile for launching in ballistic ranges (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), also by E. E. Erickson, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Supersonic aerodynamic characteristics of the Active Laser Seeker (ALS) configuration of a proposed maneuvering air-to-air missile design (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Karman Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by D. H. Fikes, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Supersonic wind tunnel tests of the IDS 6208 rocket sled (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Leroy M. Jenke, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Support interference on an ogive-cylinder model at high angle of attack in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnet Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by M. C. Altstatt, W. E. Dietz, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: A survey of transition research at AEDC (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1977., 1977), also by Jack D. Whitfield, N. Sam Dougherty, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Tables of thermodynamic properties of air in chemical equilibrium including second virial corrections from 1500⁰ K to 15,000⁰ K (Arnold Engineering Development Center, 1965), also by United States. National Bureau of Standards, Max Klein, and Joseph Hilsenrath (page images at HathiTrust)
• Arnold Engineering Development Center: Tables of thermodynamic properties of air in chemical equilibrium including second virial corrections from 1500°K to 15,000°K (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by Joseph Hilsenrath, Max Klein, and United States. National Bureau of Standards (page images at HathiTrust)
• Arnold Engineering Development Center: Tests of the Kaman KRC-6M rotochute at transonic speeds (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), also by R. D. Herron, T. W. Binion, Inc ARO, Kaman Aircraft Corporation, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Arnold Engineering Development Center: Tests of the ONERA calibration models in three transonic wind tunnels (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Travis W. Binion, United States. Air Force. Systems Command, France. Office national d'études et de recherches aérospatiales, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Theoretical and experimental studies of hypersonic viscous effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by Clark H. Lewis, Jack D. Whitfield, United States. Air Force. Arnold Air Force Base, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Three-dimensional laminar boundary-layer analysis of upwash patterns and entrained vortex formation on sharp cones at angle of attack (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by John C. Adams, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Transonic scaling effect on a quasi, two-dimensional C-141 airfoil model (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. F. Lo, W. E. Carleton, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Transonic wing/store flow-field measurement using a laser velocimeter (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), also by F. L. Heltsley, D. Brayton, F. L. Crosswy, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Two-component simultaneous LDV (Laser Doppler Velocimeter) turbulence measurements in an axisymmetric nozzle afterbody subsonic flow field with a cold, underexpanded supersonic jet (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by F. L. Heltsley, F. L. Crosswy, Calspan Field Services, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Unsteady transonic flow over blunt and pointed bodies of revolution (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Hsieh T., Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Unsteady viscous-inviscid interaction procedures for transonic airfoil flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1984., 1984), also by Tracy Donegan, United States. Air Force. Arnold Air Force Base, and Calspan Field Services (page images at HathiTrust)
• Arnold Engineering Development Center: The use of a multi-degree-of-freedom dual balance system to measure cross and cross-coupling derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1982., 1982), also by D. R. Haberman, Calspan Field Services, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Research and Development Command, United States Air Force, 1965., 1965), also by S. R. Pate, Inc ARO, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Arnold Engineering Development Center: Viscous effects on zero-lift drag of slender blunt cones (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), also by Jack D. Whitfield, B. J. Griffith, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Vorticity-stream function formulation of compressible and incompressible turbulent internal flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by John C. Chien, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: Wake properties behind an ejection seat escape system and aerodynamic characteristics with stabilization parachutes at Mach numbers from 0.6 to 1.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by David E. A. Reichenau, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. C Adams, Arloe W Mayne, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by J. C. Donaldson, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel investigation of the aerodynamic hysteresis phenomenon on the F-4 aircraft and its effects on aircraft motion (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by J. F. Herman, E. S. Washington, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel measurements of hysteresis in the static aerodynamic characteristics of aircraft (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by J. F. Herman, Inc ARO, and United States. Air Force. Arnold Air Force Base (page images at HathiTrust)
• Arnold Engineering Development Center: A Wind tunnel test to study the mutual interference of multiple bodies in the flow field of the F-4C aircraft in the transonic speed range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by A. A. Hesketh and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel testing of interactions of high altitude rocket plumes with the free stream (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by H. K. Smithson, D. L. Whitfield, L. L. Price, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel tests of a 0.06-scale B-1 model at Mach numbers from 0.60 to 1.60 : phase IV (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), also by C. J. Spurlin, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), also by H. E. McDill, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel tests of supersonic two-dimensional and half-axisymmetric inlet models in a nonuniform flow field at Mach numbers from 1.5 through 2.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1971., 1971), also by Frederick K. Hube, Leroy M. Jenke, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)
• Arnold Engineering Development Center: Wind tunnel tests of two-dimensional and half-axisymmetric inlet models at Mach numbers 1.5 through 3.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1970., 1970), also by Frederick K. Hube, Leroy M. Jenke, Inc ARO, and United States. Air Force. Systems Command (page images at HathiTrust)

See also what's at your library, or elsewhere.

Help with reading books -- Report a bad link -- Suggest a new listing

Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials

Books -- News -- Features -- Archives -- The Inside Story

Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.