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United States. Air Force. Systems Command. issuing body

Books from the extended shelves:

• United States. Air Force. Systems Command. issuing body: 0.2-scale B-1 external-compression inlet verification model test at transonic and supersonic Mach numbers : phase II /, also by R. C. German, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Ablation and viscous effects on the force and moment characteristics of slender cone models at Mach 10 under laminar flow conditions /, also by B. J. Griffith, B. M. Majors, W. T. Strike, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: AEDC high-temperature testing capabilities /, also by M. H. Trimble, R. K. Matthews, R. T. Smith, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic calibration and shakedwon testing of the full-scale F-15 aircraft inlet simulator /, also by W. F. Kinzey, E. S. Gall, V. O Williams, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Lawrence L. Galigher, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of an ejection seat escape system with a stabilization parachute at Mach numbers from 0.3 through 1.2 /, also by David E. A. Reichenau, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of low aspect ratio fins at Mach numbers from 0.80 to 1.30 /, also by D.K. Smith, R. C. German, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of perforated walls for transonic wind tunnels /, also by J. L. Jacocks, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 /, also by J. M. Whoric, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of the B-1 fuselage afterbody including simulated jet exhaust effects at Mach numbers from 0.55 to 2.20 /, also by Earl A. Price, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /, also by J. H. Jones, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by G. R. Mattasits, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Willard E. Summers, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The AFFDL-Nielsen flow-field study /, also by William T Strike, John H. Porter, Terry R. Penney, sponsor Nielsen Engineering & Research, sponsor Air Force Flight Dynamics Laboratory (U.S.), Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Afterbody drag investigation of a twin-nozzle fighter-type model at Mach numbers from 0.6 to 1.5 /, also by Earl A. Price, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Aircraft motion sensitivity to cross and cross-coupling damping derivatives /, also by R. W. Butler, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An analysis of initial static pressure probe measurements in a low-density hypervelocity wind tunnel /, also by David E. Boylan, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow /, also by John C. Adams, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analysis of three-dimensional inviscid supersonic flow between a body and an outer wall : with application to a jet stretcher system /, also by W. C. Armstrong, R. C. Bauer, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An analytic investigation of accuracy requirements for onboard instrumentation and film data for dynamically scaled wind tunnel drop models /, also by K. S. Keen, R. L. Arterbury, C. H. Morgret, Inc. Sverdrup Technology, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical and experimental thermal analysis of a guided bomb /, also by W. K. Crain, R. K. Matthews, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles /, also by T. W. Swafford, R. K. Matthews, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical description of the complete two-dimensional turbulent boundary-layer velocity profile /, also by David L. Whitfield, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical nodel of supersonic, turbulent, near-wake flows /, also by C. E. Peters, W. J. Phares, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical, numerical, and experimental results on turbulent boundary layers /, also by David L. Whitfield, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An analytical study of hypersonic inlets in free-molecule flow /, also by M. Kinslow, M. R. Busby, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Analytical study of ventilated wind tunnel boundary interference on V/STOL models including wake curvature and decay effects /, also by E. M. Kraft, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Application of splines to the numerical solution of two-point boundary-value problems /, also by Donald C. Todd, John C Adams, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An application of the Chapman-Korst theory to supersonic nozzle-afterbody flows /, also by R. C. Bauer, J. H. Fox, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Application of the vortex-lattice method to represent a jet exhausting from a flat plate into a crossflowing stream /, also by F. L. Heltsley, R. L. Parker, sponsor Martin Marietta Corporation, sponsor McDonnell Douglas Corporation, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An approximate analysis of the shock structure in underexpanded plumes /, also by C. E. Peters, W. J. Phares, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Artificially induced boundary-layer transition on blunt-slender cones using distributed roughness and spherical-type tripping devices at hypersonic speeds /, also by A. H. Boudreau, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by C. F. Anderson, F. M. Jackson, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Boundary-layer characteristics at Mach numbers 2 through 5 in the test section of the 12-inch supersonic tunnel /, also by D. R. Bell, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Boundary-layer transition correlation on a slender cone in wind tunnels and flight for indications of flow quality /, also by N. Sam Dougherty, David F. Fisher, sponsor Hugh L. Dryden Flight Research Center, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Boundary-layer transition on cones near Mach one in an aeroballistic range /, also by J. Leith Potter, J. R. Myers, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calculation of interference for a porous wall wind tunnel by the method of block cyclic reduction /, also by C. F. Lo, H. N. Glassman, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Arloe W. Mayne, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calculation of the boundary-layer growth in a Ludwieg tube /, also by James C. Sivells, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calibration and performance of the AEDC/VKF Tunnel C, Mach Number 4, Aerothermal Wind Tunnel /, also by W. T. Strike, sponsor Calspan Field Services, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /, also by F. M. Jackson, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion test section at various Reynolds numbers /, also by F. M. Jackson, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Calibration tests of a Litton conical air data probe at Mach numbers of 2 to 8 /, also by Scott R. Mallard, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Captive aircraft testing at high angles of attack /, also by R. W. Butler, J. P. Christopher, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Characteristic boundary conditions for ARO-1 /, also by Karl R. Kneile, James L. Jacocks, Donald C. Todd, sponsor Calspan Field Services, Inc. Sverdrup Technology, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Characteristics of axisymmetric and two-dimensional isoenergetic jet mixing zones /, also by R. C. Bauer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Chemical kinetic regimes of hypersonic flight simulation /, also by Donald J. Harney and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Cluster formation in free-jet expansions /, also by A. B. Bailey, R. Dawbarn, M. R. Busby, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Comments on the use of measurements of the effective moment parameter (C m alpha) /, also by C. J. Welsh, sponsor Calspan Field Services, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Commercial supersonic tansport panel flutter studies /, also by C. H. Hodson, J. E. Stocker, North American Aviation. sponsor, United States. Federal Aviation Agency. sponsor, and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data /, also by E. E. Edenfield, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by D. W Hill, R. H. Tolbert, J. T. Best, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels /, also by C. J. Schueler, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Comparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests /, also by R. E. Dix, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Comparisons of free-flight and wind tunnel data on slender cones /, also by B. J. Griffith, Leo G. Siler, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings., also by G. R. Gomillion, sponsor Air Force Armament Laboratory (U.S.), Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Computation of axisymmetric separated nozzle-afterbody flow /, also by James L. Jacocks, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A computer study of hypersonic laminar boundary-layer/shock-wave interaction using the time-dependent compressible Navier-Stokes equations /, also by B. K. Hodge, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Corrections to single-shielded total temperature probes in subsonic, supersonic, and hypersonic flow /, also by M. O. Varner, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Correlation of experimental and theoretical steady-state spinning motion for a current fighter airplane using rotation-balance aerodynamic data /, also by T. F. Langham, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Bob L. Uselton, Fred B. Cyran, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Database for internal store carriage and jettison., also by R. E. Dix, T. W. Dobson, Calspan Corporation. sponsor, Air Force Armament Laboratory (U.S.). sponsor, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by J. M. Wright, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels : theory and application /, also by Samuel R. Pate, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Drag and stability of cross type parachutes /, also by R. J. Niccum, Robert Gutenkauf, E. L. Haak, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Dynamic stability characteristics of a10-deg cone at Mach number 10 /, also by A. E. Hodapp, G. E. Burt, B. L. Uselton, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The effect of plenum volume on the test section flow characteristics of a perforated wall transonic tunnel /, also by C. F. Anderson, O. P. Credle, A. Anderson, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The effect of pressure pulsations and vibrations on fully developed pipe flow /, also by Donald O. Barnett, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Effect of shock impingement on the heat-transfer and pressure distributions on a cylindrical-leading-edge model at Mach number 19 /, also by L. G. Siler, H. E. Deskins, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Effects of acoustic and vortical disturbances on the turbulent boundary layer at free-stream Mach number 0.5 /, also by John A. Benek, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Effects of wall cooling and leading-edge blunting on ramp-induced, laminar flow separations at Mach numbers from 3 through 6 /, also by J. Don Gray, G. L. Winchenbach, R. W. Rhudy, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Engineering model of unsteady flow in a cavity /, also by R. C. Bauer, R. E. Dix, sponsor Calspan Corporation, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Equations and charts for the evaluation of the hypersonic aerodynamic characteristics of lifting configurations by the Newtonian theory /, also by E. L. Clark, L. L. Trimmer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Equations for store separation motion simulations and instrumented model data reduction /, also by K. S. Keen, sponsor Calspan Corporation, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of a method for computation of separated, turbulent, compressible boundary layers /, also by M. C. Altstatt, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of an internal balance-supporting bracket simulating lug suspension for captive stores in wind tunnel tests /, also by R. E. Dix, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers /, also by L. L. Galigher, R. C. Bauer, Steven F. Yaros, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Frederick B. Cyran, Edward J. Marquart, Bob L. Uselton, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers /, also by William Lee Peters, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of Reynolds number and tunnel wall porosity effects on nozzle afterbody drag at transonic mach numbers /, also by C. E. Robinson, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of the aerodynamic interference of the tunnel 4T Captive Trajectory System on the separation characteristics of the BLU-27 store /, also by Wallace Luchuk, David W Hill, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 /, also by Lawrence L. Galigher, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Excitation processes in ceramics and the anomalous increase in thermal conductivity at elevated temperatures /, also by D. H. Whitmore, Ill.). sponsor Northwestern University (Evanston, and United States. Air Force. Systems Command. Aeronautical Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range /, also by C. E. Robinson, M. Dean High, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow /, also by C. E. Robinson, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An experimental and analytic investigation of a transonic shock-wave/boundary-layer interaction /, also by M. C. Alstatatt, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental and theoretical study of cavity acoustics /, also by R. E. Dix, R. C. Bauer, Inc. Sverdrup Technology, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental determination of aerodynamic drag on a blunted 10-deg cone at angles of attack in hypersonic, rarefied flow /, also by David E. Boylan, William H. Sims, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental determination of the apparent moment of inertia of parachutes /, also by Shukry K. Ibrahim, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow /, also by J. Leith Potter, John T. Miller, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An experimental investigation of ducted, reactive, turbulent jet mixing with recirculation./, also by D. E. Chriss, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental investigation of the effect of various scaling laws on the quality of the free-drop store separation simulation /, also by R. A. Paulk, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental method for correcting nozzle afterbody drag for the effects of jet temperature /, also by W. L. Peters, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental studies of high temperature hypersonic diffusers /, also by Richard T. Smith and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experimental studies of the unstedy aerodynamics of panels at or near flutter with a finite boundary layer Mach number 1 to 10 /, also by G. W. Asher, A. W. Brown, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Boeing Aerospace Company. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics /, also by R. F. Starr, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flat-plate boundary-layer transition at hypersonic speeds /, also by R. E. Deem, J. S. Murphy, C. R. Erickson, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flight evaluation of various short period dynamics at four drag configurations for the landing approach task /, also by Charles R. Chalk, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Cornell Aeronautical Laboratory. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flow characteristics of a 12-in. intermittent supersonic tunnel /, also by A. Anderson, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by R. H. Roberts, J. R. Myers, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flow-field study about a hemisphere-cylinder in the transonic and low supersonic Mach number range /, also by T. Hsieh, B. M. Majors, W. T. Strike, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flow visualization photographs of a yawed tangent ogive cylinder at Mach number 2 /, also by J. H. Jones, J. E. O'Hare, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Flow visualization techniques for use in hypersonic wind tunnels /, also by R. W. Rhudy, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Force and pressure tests of an AGARD Calibration Model B at a Mach number of 10 /, also by R. K. Matthews, L. L Trimmer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Force and pressure tests on cones with simulated ablated noses at Mach numbers 8 and 16 /, also by J. S. Hahn, H. R. Little, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Force tests of standard hypervelocity ballistic models HB-1 and HB-2 at Mach 1.5 to 10 /, also by J. Don Gray, E. Earl Lindsay, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Free-flight investigation of ablation effects n the stability of conical reentry configurations /, also by C. J. Welsh, G. L. Winchenbach, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Free turbulent mixing : a critical evaluation of theory and experiment /, also by Philip Thomas Harsha, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Fundamental studies of subsonic and transonic flow separation., also by J. M. 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. sponsor, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Further experiments on impact-pressure probes in a low-density, hypervelocity flow /, also by A. B. Bailey, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Heat-transfer and flow-field tests of the McDonnell Douglas-Martin Marietta space shuttle configurations /, also by R. K. Matthews, R. H. Eaves, W. R. Martindale, sponsor Martin Marietta Corporation, sponsor McDonnell Douglas Corporation, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Heat-transfer and flow-field tests of the North American Rockwell/ General Dynamics Convair space shuttle configurations /, also by W. R. Martindale, L. L. Trimmer, R. K. Matthews, sponsor North American Rockwell Corporation, sponsor General Dynamics Corporation. Convair Division, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 /, also by M. E. Hillsamer, J. P. Rhudy, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: High alpha aerodynamics /, also by Inc ARO and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Holographic interferometry measurements of subsonic turbulent boundary layers /, also by D. W. Sinclair, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Hypersonic dynamic stability, also by R. B. Hobbs, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and General Electric Company. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Hypersonic dynamic stability., also by L. A. Marshall and Air Force Flight Dynamics Laboratory (U.S.). sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Hypersonic force, pressure, and heat transfer investigations of sharp and blunt slender cones /, also by David B. Wilkinson, Shelby A. Harrington, sponsor Cornell Aeronautical Laboratory, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Hypersonic lifting body windward surface flow-field analysis for high angles of incidence /, also by John C. Adams, William R. Martindale, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The influence of slight leading-edge bluntness on boundary-layer transition at a Mach number of eight /, also by Jack D. Whitfield, J. Leith Potter, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An influence of the orifice on measured pressures in rarefied flow /, also by J. Leith Potter, David E. Boylan, Max Kinslow, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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., also by N. Sam Dougherty, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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., also by N. Sam Dougherty, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Influences of sting support on aerodynamic loads acting on captive store models /, also by R. E. Dix, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Influences of sway braces and mounting gaps on the static aerodynamic loading of external stores /, also by R. E. Dix, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Injection of particles through a jet nozzle laterally into a supersonic airstream /, also by E. E. Hilliard, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Inlet performance characteristics of a 1/5 scale Northrop YF-17 model at transonic and supersonic Mach numbers /, also by M. E. Sanders, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Inlet performance characteristics of a generalized 1/4-scale tactical aircraft models at transonic and supersonic Mach numbers /, also by R. F. Lauer, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Inlet performance characteristics of a generalized 1/5.2-scale aircraft model at transonic and supersonic Mach numbers /, also by Jimmy Walker, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Integral analysis of ducted two-stream mixing with recirculation /, also by C. E. Peters, W. J. Phares, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An integral equation method for boundary interference in a perforated-wall wind tunnel at transonic speeds /, also by E. M. Kraft, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Integral solution of compressible turbulent boundary layers using improved velocity profiles /, also by David L. Whitfield, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Interactions produced by sonic lateral jets located on surface in a supersonic stream /, also by W. T. Strike, J. S. Deitering, C. J. Schueler, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Interference on a model afterbody from downstream support hardware at transonic Mach numbers /, also by Earl A. Price, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers /, also by A. V. Spratley, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of an upper stage rocket plane with external-burning thrust augmentation /, also by E. E. Callens, J. Leith Potter, J. T. Miller, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4 /, also by S. R. Pate, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of ducted, two-stream, variable-density, turbulent jet mixing with recirculation /, also by Roy J. Schulz, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference /, also by Earl A. Price, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of flow separation on a two-dimensional flat plate haveing a variable-san trailing-edge flap at M [free stream] = 3 and 5 /, also by S. R. Pate, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by T. Hsieh, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 /, also by A. L. Baer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model /, also by Travis W. Binion, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of sting interference effects on an oscillating cone in transonic flow /, also by Frederick B. Cyran, J. P. Christopher, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of subsonic annular nozzles for engine exhaust/external flow interaction studies /, also by R. J. Matz, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of the effects of nose bluntness on natural and induced boundary-layer transition on axisymmetric bodies in supersonic flow /, also by Jack D. Coats, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers /, also by T. O. Shadow, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of various textile parachutes and control systems to achieve steerability /, also by V. F. Riley, E. M. Linhart, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Northrop Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Investigation of various textile parachutes and control systems to achieve steerability : Phases III and IV /, also by E. M. Linhart, C. R. Graham, V. F. Riley, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Northrop Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Inviscid and viscous hypersonic nozzle flow with finite rate chemical reactions /, also by E. S. Levinsky, Jerome James Brainerd, sponsor General Dynamics Corporation. Astronautics Division, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Inviscid blunt leading effects on planar surface pressure distributions at Mach number 10 /, also by W. T. Strike, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Jet simulation techniques : simulation of temperature effects by altering gas composition /, also by W. L. Peters, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds /, also by J. Don Gray, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow /, also by David E. Boylan, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Laser-Raman flow-field diagnostics of two large hypersonic test facilities /, also by W. D. Williams, L. L. Price, H. M. Powell, D. A. Wagner, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Longitudinal force charactristics of two AFFDL MDF-4 high lift-to-drag configurations at Mach number 19 /, also by A. R. Wallace, L. G. Siler, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by F. J. Keeney, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Low-density boundary-layer modulation by suction in a hypersonic nozzle /, also by M. Kinslow, J. Leith Potter, M. R. Busby, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Low-density hypervelocity wind tunnel diffuser performance /, also by M. W. Milligan, J. F. Bailey, Knoxville. Department of Mechanical and Aerospace Engineering niversity of Tennessee, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A magnetic-guideway/guided-projectile system concept for aeroballistic ranges /, also by George D Arney, Charles W Pender, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Measurement of the pressure fluctuations in the test section of the 1-foot transonic tunnel in the frequency range from 5 to 1250 cps /, also by J. E. Robertson, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A mehod for the prediction of the effects of free-stream disturbances on boundary-layer transition /, also by J. A. Benek, M. Dean High, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Method for calculation of the one-dimensional nonequilibrium flow of a general gas mixture through a hypersonic nozzle /, also by George Emanuel, Walter G. Vincenti, sponsor Stanford University. Department of Aeronautics and Astronautics, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A method for estimating jet entrainment effects on nozzle-afterbody drag /, also by R. C. Bauer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A method of characteristics computer program for three-dimensional supersonic internal flows /, also by W. C. Armstrong, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Missile motion sensitivity to dynamic stability derivatives /, also by T. F. Langham, E. S. Washington, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel /, also by J. E. Robertson, sponsor Wyle Laboratories, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Modifications to MacCormack's 2-D Navier-Stokes compression ramp code for application to flows with axes of symmetry and wall mass transfer /, also by Richard G. Hindman, Edward J. Marquart, Bob L. Uselton, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Nacelle afterbody drag investigation of a B-1 0.06-scale model at Mach numbers from 0.55 to 2.2 /, also by M. L. Homan, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: NEQPAK, the AEDC thermochemical nonequilibrium package : theory and use /, also by J. T. Curtis, R. W. Tramel, sponsor Calspan Corporation, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Noise generation in transonic wind tunnels /, also by M. O. Varner, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Nonlinear thermoelastic effects on hypersonic stability and control., also by James R. Batt, Air Force Flight Dynamics Laboratory (U.S.). sponsor, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Nonlinear thermoelastic effects on hypersonic stability and control., also by James R. Batt, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Wright-Patterson Air Force Base. Flight Dynamics Laboratory (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Nonlinear thermoelastic effects on hypersonic stability and control., also by James R. Batt, Richard H. Gallagher, Air Force Flight Dynamics Laboratory (U.S.). sponsor, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Bell Aircraft Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Numerical analysis of recirculating ducted flows /, also by R. J. Schulz, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Numerical analysis of turbulent separated subsonic diffuser flows /, also by J. C. Chien, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil /, also by John C. Adams, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Numerical computation of subsonic conical diffuser flows with nonuniform turbulent inlet conditions /, also by J. C. Chien, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Numerical stability analysis of a compressor model /, also by K. C. Reddy, Yeng-Yung Tsui, sponsor University of Tennessee (System). Space Institute, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: PEGSUS 4.0 User's Manual /, also by N. E. Suhs, R. W. Tramel, sponsor Calspan Corporation, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels /, also by O. P. Credle, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls., also by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Grumman Aircraft Engineering Corporation. Research Department. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Pressure distribution and flow visualization tests of a 1.5 elliptic cone at Mach 10 /, also by R. L. Palko, A. D. Ray, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Pressure measurements for Mach five flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and control characteristics /, also by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Grumman Aircraft Engineering Corporation. Research Department. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls., also by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Grumman Aircraft Engineering Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Pressure tests on the standard hypervelocity ballistic model HB-2 at Mach 1.5 to 5 /, also by Jerry H. Jones, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Problems underlying the numerical integration of the chemical and vibrational rate equations in a near-equilibrium flow /, also by George Emanuel, sponsor Stanford University. Department of Aeronautics and Astronautics, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Research on adaptive wall wind tunnels /, also by Robert J. Vidal, J. C Erickson, sponsor Arnold Engineering Development Center, and sponsor Calspan Corporation (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Results of a 0.1-scale B-1 inlet model test at transonic and supersonic Mach numbers /, also by F. J. Graham, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Results of a 0.2-scale B-1 inlet verification model test at transonic and supersonic Mach numbers /, also by John F. Riddell, F. M. Jackson, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Results of the full-scale F-15 inlet/engine compatibility test at subsonic and supersonic Mach numbers /, also by H. E. McDill, J. L. Jacocks, R. F. Lauer, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Roll-damping derivative calculations for spinning sharp and blunt cones in supersonic and hypersonic flow /, also by Arloe W. Mayne, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies., also by John A. Benek, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Shock-fitting for full potential equation /, also by M. M. Hafez, Earll M. Murman, sponsor Arnold Engineering Development Center, and inc. Flow Research (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The shock shape and shock detachment distance for spheres and flat-faced bodies in low-density, hypervelocity, argon flow /, also by A. B. Bailey, W. H. Sims, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Simplified input for certain aerodynamic nose configurations to the Grumman QUICK-geometry system : a KWIKNOSE User's Manual /, also by Frederick L. Shope, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Skin-friction measurements at subsonic and transonic Mach numbers with embedded-wire gages /, also by D. W. Sinclair, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Solution for the transient one-dimensional heat conduction in an infinite slab /, also by John T Miller, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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., also by William B. Baker, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Static force tests at Mach 8 of sharp and blunt 20-deg half-angle cones with a blunt 70-deg swept delta wing /, also by G. H. Merz, O. R. Pritts, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Static pressure on sharp and blunt cones in conical and parallel low-density flow /, also by Max Kinslow, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Static stability and drag characteristics of a hypersonic aircraft design at Mach numbers 1.5 to 5.6 /, also by J. T. Jr Best, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Static stability and drag characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /, also by J. T. Best, R. W. Rhudy, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Sting dynamics of wind tunnel models /, also by James P. Billingsley, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Sting interference effects as determined by measurements of dynamic stability derivatives, surface pressure, and base pressure for Mach numbers 2 through 8 /, also by Bob L. Uselton, Frederick B. Cyran, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Sting interference effects on the Modified Basic Finner Missile at Mach numbers 0.3 through 1.3 /, also by Edward J. Marquart, sponsor Calspan Field Services, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Store separation testing techniques at the Arnold Engineering Development Center., also by J. P. Billingsley, J. T. Best, R. H. Burt, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Store separation testing techniques at the Arnold Engineering Development Center., also by E. G Allee, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Store separation testing techniques at the Arnold Engineering Development Center., also by J. B. Carman, J. P. Christopher, D. W. Hill, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Store separation testing techniques at the Arnold Engineering Development Center., also by J. B. Carman, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Stress analysis of a parachute during inflation and at steady state /, also by H. G. Heinrich, Lelan R. Jamison, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and University of Minnesota. Department of Aerospace Engineering and Mechanics. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls /, also by N. Sam Dougherty, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Subsonic characteristics of low aspect ratios., also by Eugene L. Crosthwait, Donald D. Seath, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and General Dynamics Corporation. Fort Worth Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Subsonic characteristics of low aspect ratios., also by J. K. Beamish, Eugene L. Crosthwait, G. J. Klein, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and General Dynamics Corporation. Fort Worth Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Summary report on aerodynamic characteristics of standard models HB-1 and HB-2 /, also by J. Don Gray, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A superconducting magnet dewar missile for launching in ballistic ranges /, also by E. E. Erickson, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Supersonic aerodynamic characteristics of the Active Laser Seeker (ALS) configuration of a proposed maneuvering air-to-air missile design /, also by D. H. Fikes, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Support interference on an ogive-cylinder model at high angle of attack in transonic flow /, also by M. C. Altstatt, W. E. Dietz, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: A survey of transition research at AEDC /, also by Jack D. Whitfield, N. Sam Dougherty, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Tests of the ONERA calibration models in three transonic wind tunnels /, also by Travis W. Binion, sponsor Arnold Engineering Development Center, sponsor France. Office national d'études et de recherches aérospatiales, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Three-dimensional laminar boundary-layer analysis of upwash patterns and entrained vortex formation on sharp cones at angle of attack /, also by John C. Adams, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Transonic scaling effect on a quasi, two-dimensional C-141 airfoil model /, also by C. F. Lo, W. E. Carleton, Arnold Engineering Development Center. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Transonic wing/store flow-field measurement using a laser velocimeter /, also by F. L. Heltsley, D. Brayton, F. L. Crosswy, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Two-component simultaneous LDV turbulence measurements in an axisymmetric nozzle afterbody subsonic flow field with a cold, underexpanded supersonic jet /, also by F. L. Heltsley, F. L. Crosswy, sponsor Calspan Field Services, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Unsteady aerodynamics for advanced configurations., also by M. T. Moore, L. V. Andrew, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Unsteady aerodynamics for advanced configurations., also by H. T. Vivian, L. V. Andrew, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Unsteady aerodynamics for advanced configurations., also by T. C. Li, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Unsteady aerodynamics for advanced configurations., also by E. R. Rodemich, L. V. Andrew, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Unsteady aerodynamics for advanced configurations., also by E. Albano, L. V. Andrew, Air Force Flight Dynamics Laboratory (U.S.). sponsor, Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and North American Aviation. Space and Information Systems Division. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: The use of a multi-degree-of-freedom dual balance system to measure cross and cross-coupling derivatives /, also by D. R. Haberman, sponsor Calspan Field Services, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Viscous effects on zero-lift drag of slender blunt cones /, also by Jack D. Whitfield, B. J. Griffith, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wake properties behind an ejection seat escape system and aerodynamic characteristics with stabilization parachutes at Mach numbers from 0.6 to 1.5 /, also by David E. A. Reichenau, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers /, also by J. C Adams, Arloe W Mayne, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel investigation of aerodynamic loads on weapons separated from carriage under the wing of a tactical fighter aircraft at supersonic speeds /, also by J. C. Donaldson, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel investigation of the aerodynamic hysteresis phenomenon on the F-4 aircraft and its effects on aircraft motion /, also by J. F. Herman, E. S. Washington, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel testing of interactions of high altitude rocket plumes with the free stream /, also by H. K. Smithson, D. L. Whitfield, L. L. Price, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel tests of a 0.06-scale B-1 model at Mach numbers from 0.60 to 1.60 : phase IV /, also by C. J. Spurlin, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine /, also by H. E. McDill, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: 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 /, also by Frederick K. Hube, Leroy M. Jenke, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. issuing body: Wind tunnel tests of two-dimensional and half-axisymmetric inlet models at Mach numbers 1.5 through 3.0 /, also by Frederick K. Hube, Leroy M. Jenke, Inc. ARO, and Arnold Engineering Development Center. sponsor (page images at HathiTrust)

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