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Online Books by

Inc. ARO

(ARO, Inc., sponsor)

Books from the extended shelves:

• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: AEDC high-temperature testing capabilities /, also by M. H. Trimble, R. K. Matthews, R. T. Smith, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Aerodynamic characteristics of perforated walls for transonic wind tunnels /, also by J. L. Jacocks, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 /, also by J. M. Whoric, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Aerodynamic characteristics of the HAST missile at Mach numbers 2.25, 3.0, and 4.0 /, also by J. H. Jones, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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.), Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Aircraft motion sensitivity to cross and cross-coupling damping derivatives /, also by R. W. Butler, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An analysis of initial static pressure probe measurements in a low-density hypervelocity wind tunnel /, also by David E. Boylan, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical and experimental thermal analysis of a guided bomb /, also by W. K. Crain, R. K. Matthews, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles /, also by T. W. Swafford, R. K. Matthews, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical description of the complete two-dimensional turbulent boundary-layer velocity profile /, also by David L. Whitfield, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical nodel of supersonic, turbulent, near-wake flows /, also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical, numerical, and experimental results on turbulent boundary layers /, also by David L. Whitfield, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An analytical study of hypersonic inlets in free-molecule flow /, also by M. Kinslow, M. R. Busby, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Analytical study of ventilated wind tunnel boundary interference on V/STOL models including wake curvature and decay effects /, also by E. M. Kraft, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Application of linearized transonic theory to tunnel blockage interference /, also by C. F. Lo, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Application of splines to the numerical solution of two-point boundary-value problems /, also by Donald C. Todd, John C Adams, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An application of the Chapman-Korst theory to supersonic nozzle-afterbody flows /, also by R. C. Bauer, J. H. Fox, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An approximate analysis of the shock structure in underexpanded plumes /, also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Boundary-layer transition under hypersonic conditions /, also by J. Leith Potter, Jack D. Whitfield, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Calculation of the boundary-layer growth in a Ludwieg tube /, also by James C. Sivells, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Calibration of the AEDC-PWT 16-Foot transonic tunnel aerodynamic test section at various Reynolds numbers /, also by F. M. Jackson, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Calibration of the AEDC-PWT 16-ft transonic tunnel with the propulsion test section at various Reynolds numbers /, also by F. M. Jackson, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Calibration tests of a Litton conical air data probe at Mach numbers of 2 to 8 /, also by Scott R. Mallard, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Captive aircraft testing at high angles of attack /, also by R. W. Butler, J. P. Christopher, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Characteristics of axisymmetric and two-dimensional isoenergetic jet mixing zones /, also by R. C. Bauer, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Cluster formation in free-jet expansions /, also by A. B. Bailey, R. Dawbarn, M. R. Busby, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data /, also by E. E. Edenfield, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: A comparison of transition Reynolds numbers from 12-in. and 40-in. supersonic tunnels /, also by C. J. Schueler, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Comparison of two methods used to measure aerodynamic loads acting on captive store models in wind tunnel tests /, also by R. E. Dix, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Comparisons of free-flight and wind tunnel data on slender cones /, also by B. J. Griffith, Leo G. Siler, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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.), Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Computation of axisymmetric separated nozzle-afterbody flow /, also by James L. Jacocks, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: A computer study of hypersonic laminar boundary-layer/shock-wave interaction using the time-dependent compressible Navier-Stokes equations /, also by B. K. Hodge, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Corrections to single-shielded total temperature probes in subsonic, supersonic, and hypersonic flow /, also by M. O. Varner, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Correlation of experimental and theoretical steady-state spinning motion for a current fighter airplane using rotation-balance aerodynamic data /, also by T. F. Langham, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels : theory and application /, also by Samuel R. Pate, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Dynamic stability characteristics of a10-deg cone at Mach number 10 /, also by A. E. Hodapp, G. E. Burt, B. L. Uselton, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: The effect of pressure pulsations and vibrations on fully developed pipe flow /, also by Donald O. Barnett, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Effects of acoustic and vortical disturbances on the turbulent boundary layer at free-stream Mach number 0.5 /, also by John A. Benek, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Evaluation of a method for computation of separated, turbulent, compressible boundary layers /, also by M. C. Altstatt, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Evaluation of an internal balance-supporting bracket simulating lug suspension for captive stores in wind tunnel tests /, also by R. E. Dix, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers /, also by William Lee Peters, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range /, also by C. E. Robinson, M. Dean High, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow /, also by C. E. Robinson, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An experimental and analytic investigation of a transonic shock-wave/boundary-layer interaction /, also by M. C. Alstatatt, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An experimental investigation of ducted, reactive, turbulent jet mixing with recirculation./, also by D. E. Chriss, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Experimental method for correcting nozzle afterbody drag for the effects of jet temperature /, also by W. L. Peters, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Experiments to assess the influence of changes in the tunnel wall boundary layer on transonic wall crossflow characteristics /, also by R. F. Starr, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Flow characteristics of a 12-in. intermittent supersonic tunnel /, also by A. Anderson, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Flow visualization techniques for use in hypersonic wind tunnels /, also by R. W. Rhudy, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Free-flight investigation of ablation effects n the stability of conical reentry configurations /, also by C. J. Welsh, G. L. Winchenbach, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Free turbulent mixing : a critical evaluation of theory and experiment /, also by Philip Thomas Harsha, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Further experiments on impact-pressure probes in a low-density, hypervelocity flow /, also by A. B. Bailey, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 /, also by M. E. Hillsamer, J. P. Rhudy, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Holographic interferometry measurements of subsonic turbulent boundary layers /, also by D. W. Sinclair, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Hypersonic lifting body windward surface flow-field analysis for high angles of incidence /, also by John C. Adams, William R. Martindale, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An influence of the orifice on measured pressures in rarefied flow /, also by J. Leith Potter, David E. Boylan, Max Kinslow, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Influences of sting support on aerodynamic loads acting on captive store models /, also by R. E. Dix, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Influences of sway braces and mounting gaps on the static aerodynamic loading of external stores /, also by R. E. Dix, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Injection of particles through a jet nozzle laterally into a supersonic airstream /, also by E. E. Hilliard, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Inlet performance characteristics of a 1/5 scale Northrop YF-17 model at transonic and supersonic Mach numbers /, also by M. E. Sanders, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Inlet performance characteristics of a generalized 1/4-scale tactical aircraft models at transonic and supersonic Mach numbers /, also by R. F. Lauer, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Inlet performance characteristics of a generalized 1/5.2-scale aircraft model at transonic and supersonic Mach numbers /, also by Jimmy Walker, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Integral analysis of ducted two-stream mixing with recirculation /, also by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Integral solution of compressible turbulent boundary layers using improved velocity profiles /, also by David L. Whitfield, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Interference on a model afterbody from downstream support hardware at transonic Mach numbers /, also by Earl A. Price, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An investigaion of boattail geometry and Reynolds number effects on forebody and afterbody drag at transonic Mach numbers /, also by A. V. Spratley, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of ducted, two-stream, variable-density, turbulent jet mixing with recirculation /, also by Roy J. Schulz, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of F-16 nozzle-afterbody forces at transonic Mach numbers with emphasis on support system interference /, also by Earl A. Price, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of separated flows on two-dimensional models at Mach numbers 5 and 8 /, also by A. L. Baer, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of several slotted wind tunnel wall configurations with a high disk loading V/STOL model /, also by Travis W. Binion, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of sting interference effects on an oscillating cone in transonic flow /, also by Frederick B. Cyran, J. P. Christopher, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Investigation of subsonic annular nozzles for engine exhaust/external flow interaction studies /, also by R. J. Matz, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers /, also by T. O. Shadow, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: An Investigation of three-dimensional wall interference in a variable porosity transonice wind tunnel /, also by Travis W. Binion, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Inviscid blunt leading effects on planar surface pressure distributions at Mach number 10 /, also by W. T. Strike, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Jet simulation techniques : simulation of temperature effects by altering gas composition /, also by W. L. Peters, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Laminar boundary-layer separation on flared bodies at supersonic and hypersonic speeds /, also by J. Don Gray, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow /, also by David E. Boylan, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: A magnetic-guideway/guided-projectile system concept for aeroballistic ranges /, also by George D Arney, Charles W Pender, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: A method for estimating jet entrainment effects on nozzle-afterbody drag /, also by R. C. Bauer, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: A method of characteristics computer program for three-dimensional supersonic internal flows /, also by W. C. Armstrong, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Missile motion sensitivity to dynamic stability derivatives /, also by T. F. Langham, E. S. Washington, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Noise generation in transonic wind tunnels /, also by M. O. Varner, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Numerical analysis of recirculating ducted flows /, also by R. J. Schulz, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Numerical analysis of turbulent separated subsonic diffuser flows /, also by J. C. Chien, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Numerical calculation of the subsonic and transonic turbulent boundary layer on an infinite yawed airfoil /, also by John C. Adams, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Numerical computation of subsonic conical diffuser flows with nonuniform turbulent inlet conditions /, also by J. C. Chien, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Perforated wall noise in the AEDC-PWT 16-ft and 4-ft transonic tunnels /, also by O. P. Credle, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Pressure distribution and flow visualization tests of a 1.5 elliptic cone at Mach 10 /, also by R. L. Palko, A. D. Ray, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Pressure tests on the standard hypervelocity ballistic model HB-2 at Mach 1.5 to 5 /, also by Jerry H. Jones, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Real gas scale effects on hypersonic laminar boundary-layer parameters including effects of entropy-layer swallowing /, also by J. C. Adams, E. O. Marchand, A. W. Mayne, W. R. Martindale, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Results of a 0.1-scale B-1 inlet model test at transonic and supersonic Mach numbers /, also by F. J. Graham, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Roll-damping derivative calculations for spinning sharp and blunt cones in supersonic and hypersonic flow /, also by Arloe W. Mayne, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies., also by John A. Benek, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Simplified input for certain aerodynamic nose configurations to the Grumman QUICK-geometry system : a KWIKNOSE User's Manual /, also by Frederick L. Shope, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Skin-friction measurements at subsonic and transonic Mach numbers with embedded-wire gages /, also by D. W. Sinclair, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Solution for the transient one-dimensional heat conduction in an infinite slab /, also by John T Miller, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Static pressure on sharp and blunt cones in conical and parallel low-density flow /, also by Max Kinslow, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Sting dynamics of wind tunnel models /, also by James P. Billingsley, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Store separation testing techniques at the Arnold Engineering Development Center., also by J. P. Billingsley, J. T. Best, R. H. Burt, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Store separation testing techniques at the Arnold Engineering Development Center., also by E. G Allee, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Store separation testing techniques at the Arnold Engineering Development Center., also by J. B. Carman, J. P. Christopher, D. W. Hill, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Store separation testing techniques at the Arnold Engineering Development Center., also by J. B. Carman, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: A study of acoustic disturbances and means of suppression in ventilated transonic wind tunnel walls /, also by N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Summary report on aerodynamic characteristics of standard models HB-1 and HB-2 /, also by J. Don Gray, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: A superconducting magnet dewar missile for launching in ballistic ranges /, also by E. E. Erickson, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Supersonic aerodynamic characteristics of the Active Laser Seeker (ALS) configuration of a proposed maneuvering air-to-air missile design /, also by D. H. Fikes, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Supersonic wind tunnel tests of the IDS 6208 rocket sled /, also by Leroy M. Jenke, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Support interference on an ogive-cylinder model at high angle of attack in transonic flow /, also by M. C. Altstatt, W. E. Dietz, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: A survey of transition research at AEDC /, also by Jack D. Whitfield, N. Sam Dougherty, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., sponsor: Tests of the ONERA calibration models in three transonic wind tunnels /, also by Travis W. Binion, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and sponsor France. Office national d'études et de recherches aérospatiales (page images at HathiTrust)
• ARO, Inc., sponsor: Theoretical and experimental studies of hypersonic viscous effects /, also by Clark H. Lewis, Jack D. Whitfield, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: 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 United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Transonic wing/store flow-field measurement using a laser velocimeter /, also by F. L. Heltsley, D. Brayton, F. L. Crosswy, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Viscous effects on zero-lift drag of slender blunt cones /, also by Jack D. Whitfield, B. J. Griffith, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers /, also by J. C Adams, Arloe W Mayne, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., sponsor: Wind tunnel tests of a full-scale air-launched cruise missile with an installed turbofan engine /, also by H. E. McDill, United States. Air Force. Systems Command. issuing body, and sponsor Arnold Engineering Development Center (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• ARO, Inc., 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, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)

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