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Arnold Engineering Development Center. sponsor

Books from the extended shelves:

• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /, also by J. H. Jones, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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.), United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An analysis of initial static pressure probe measurements in a low-density hypervelocity wind tunnel /, also by David E. Boylan, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Analytical and experimental thermal analysis of a guided bomb /, also by W. K. Crain, R. K. Matthews, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles /, also by T. W. Swafford, R. K. Matthews, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Analytical, numerical, and experimental results on turbulent boundary layers /, also by David L. Whitfield, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An analytical study of hypersonic inlets in free-molecule flow /, also by M. Kinslow, M. R. Busby, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Boundary-layer transition on cones near Mach one in an aeroballistic range /, also by J. Leith Potter, J. R. Myers, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Calculation of the boundary-layer growth in a Ludwieg tube /, also by James C. Sivells, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Calibration tests of a Litton conical air data probe at Mach numbers of 2 to 8 /, also by Scott R. Mallard, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Captive aircraft testing at high angles of attack /, also by R. W. Butler, J. P. Christopher, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Characteristics of axisymmetric and two-dimensional isoenergetic jet mixing zones /, also by R. C. Bauer, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Chemical kinetic regimes of hypersonic flight simulation /, also by Donald J. Harney and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Cluster formation in free-jet expansions /, also by A. B. Bailey, R. Dawbarn, M. R. Busby, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Comments on the use of measurements of the effective moment parameter (C m alpha) /, also by C. J. Welsh, sponsor Calspan Field Services, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data /, also by E. E. Edenfield, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels /, also by C. J. Schueler, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Comparisons of free-flight and wind tunnel data on slender cones /, also by B. J. Griffith, Leo G. Siler, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Computation of axisymmetric separated nozzle-afterbody flow /, also by James L. Jacocks, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: The effect of pressure pulsations and vibrations on fully developed pipe flow /, also by Donald O. Barnett, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Engineering model of unsteady flow in a cavity /, also by R. C. Bauer, R. E. Dix, sponsor Calspan Corporation, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Equations for store separation motion simulations and instrumented model data reduction /, also by K. S. Keen, sponsor Calspan Corporation, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Evaluation of a method for computation of separated, turbulent, compressible boundary layers /, also by M. C. Altstatt, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Evaluation of Reynolds number and tunnel wall porosity effects on nozzle afterbody drag at transonic mach numbers /, also by C. E. Robinson, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 /, also by Lawrence L. Galigher, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Experimental and theoretical study of cavity acoustics /, also by R. E. Dix, R. C. Bauer, Inc. Sverdrup Technology, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Experimental heat transfer to blunt axisymmetric bodies near the limit of continuum flow /, also by J. Leith Potter, John T. Miller, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Experimental investigation of the effect of various scaling laws on the quality of the free-drop store separation simulation /, also by R. A. Paulk, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Experimental method for correcting nozzle afterbody drag for the effects of jet temperature /, also by W. L. Peters, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Flow characteristics of a 12-in. intermittent supersonic tunnel /, also by A. Anderson, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Flow phenomena in starting a hypersonic shock tunnel /, also by Herbert S. Glick, William E. Smith, Abraham Hertzberg, United States. Air Force. Air Research and Development Command. sponsor, and Cornell Aeronautical Laboratory. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Flow visualization photographs of a yawed tangent ogive cylinder at Mach number 2 /, also by J. H. Jones, J. E. O'Hare, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Flow visualization techniques for use in hypersonic wind tunnels /, also by R. W. Rhudy, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Force and pressure tests on cones with simulated ablated noses at Mach numbers 8 and 16 /, also by J. S. Hahn, H. R. Little, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Free-flight investigation of ablation effects n the stability of conical reentry configurations /, also by C. J. Welsh, G. L. Winchenbach, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Free turbulent mixing : a critical evaluation of theory and experiment /, also by Philip Thomas Harsha, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Further experiments on impact-pressure probes in a low-density, hypervelocity flow /, also by A. B. Bailey, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 /, also by M. E. Hillsamer, J. P. Rhudy, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: High alpha aerodynamics /, also by Inc ARO and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Hypersonic lifting body windward surface flow-field analysis for high angles of incidence /, also by John C. Adams, William R. Martindale, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An Improved interaction method for calculating exhaust nozzle boattail flows /, also by Gary D. Kuhn, United States. Air Force. Arnold Air Force Base. sponsor, and Nielsen Engineering & Research. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: The Inertial impaction of small particles /, also by M. N. Golovin, A. A. Putnam, United States. Air Force. Air Research and Development Command. sponsor, and Battelle Memorial Institute. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An influence of the orifice on measured pressures in rarefied flow /, also by J. Leith Potter, David E. Boylan, Max Kinslow, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Influences of sting support on aerodynamic loads acting on captive store models /, also by R. E. Dix, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Injection of particles through a jet nozzle laterally into a supersonic airstream /, also by E. E. Hilliard, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An integral equation method for boundary interference in a perforated-wall wind tunnel at transonic speeds /, also by E. M. Kraft, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Interference on a model afterbody from downstream support hardware at transonic Mach numbers /, also by Earl A. Price, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An investigation of an upper stage rocket plane with external-burning thrust augmentation /, also by E. E. Callens, J. Leith Potter, J. T. Miller, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 /, also by A. L. Baer, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: An investigation of sting interference effects on an oscillating cone in transonic flow /, also by Frederick B. Cyran, J. P. Christopher, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Inviscid blunt leading effects on planar surface pressure distributions at Mach number 10 /, also by W. T. Strike, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds /, also by J. Don Gray, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Low-density boundary-layer modulation by suction in a hypersonic nozzle /, also by M. Kinslow, J. Leith Potter, M. R. Busby, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: A method for estimating jet entrainment effects on nozzle-afterbody drag /, also by R. C. Bauer, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Missile motion sensitivity to dynamic stability derivatives /, also by T. F. Langham, E. S. Washington, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Model study of the exhaust flow noise of the proposed AEDC high Reynolds number tunnel /, also by J. E. Robertson, sponsor Wyle Laboratories, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: NEQPAK, the AEDC thermochemical nonequilibrium package : theory and use /, also by J. T. Curtis, R. W. Tramel, sponsor Calspan Corporation, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Noise generation in transonic wind tunnels /, also by M. O. Varner, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil /, also by John C. Adams, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Numerical stability analysis of a compressor model /, also by K. C. Reddy, Yeng-Yung Tsui, sponsor University of Tennessee (System). Space Institute, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: PEGSUS 4.0 User's Manual /, also by N. E. Suhs, R. W. Tramel, sponsor Calspan Corporation, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels /, also by O. P. Credle, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Pressure tests on the standard hypervelocity ballistic model HB-2 at Mach 1.5 to 5 /, also by Jerry H. Jones, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Skin-friction measurements at subsonic and transonic Mach numbers with embedded-wire gages /, also by D. W. Sinclair, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Solution for the transient one-dimensional heat conduction in an infinite slab /, also by John T Miller, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Static pressure on sharp and blunt cones in conical and parallel low-density flow /, also by Max Kinslow, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Sting dynamics of wind tunnel models /, also by James P. Billingsley, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Summary report on aerodynamic characteristics of standard models HB-1 and HB-2 /, also by J. Don Gray, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: A superconducting magnet dewar missile for launching in ballistic ranges /, also by E. E. Erickson, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Tables of thermodynamic properties of air in chemical equilibrium including second virial corrections from 1500°K to 15,000°K /, also by Joseph Hilsenrath, Max Klein, and United States. National Bureau of Standards. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Transonic scaling effect on a quasi, two-dimensional C-141 airfoil model /, also by C. F. Lo, W. E. Carleton, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Transonic wing/store flow-field measurement using a laser velocimeter /, also by F. L. Heltsley, D. Brayton, F. L. Crosswy, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Viscous effects on zero-lift drag of slender blunt cones /, also by Jack D. Whitfield, B. J. Griffith, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers /, also by J. C Adams, Arloe W Mayne, Inc. ARO, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Arnold Engineering Development Center. sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)

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