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Inc.. sponsor ARO

Books from the extended shelves:

• ARO, Inc. sponsor: The AEDC three-dimensional, potential flow computer program., also by Donald C. Todd, 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: The AEDC three-dimensional, potential flow computer program., also by Richard L. Palko, 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: Aerodynamic and cold jet plume geometry characteristics of the Army free rocket at transonic mach numbers /, also by E. S. Washington, 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: Aerodynamic characteristics and store loads of a 1/24-scale F-111 aircraft model with three external store loadings /, also by C. F. Anderson and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Aircraft motion sensitivity to dynamic stability derivatives /, also by T. F. Langham, 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: Altitude-velocity table and charts for imperfect air., also by Clark H. Lewis, E. G. Burgess, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes /, also by Steven F. Yaros, 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: An Analytical study of the use of air-equivalent hot gaseous mixtures for aerodynamic test purposes /, also by Kenneth E. Tempelmeyer, Arnold Engineering Development Center. issuing body, and United States. Air Force. Air Research and Development Command. sponsor (page images at HathiTrust)
• ARO, Inc. sponsor: Applications of the aerotherm BLIMP boundary-layer program to nonablating reentry flight conditions /, also by Emmett E. Edenfield, 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: Calculation of skin friction intwo-dimensional, transonic, turbulent flow /, also by T. W. Swafford, 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: Combined effects of viscous interaction and ideal source flow on pressure and heat-transfer distributions over hemisphere cylinders at M infinity is approximately 18 /, also by R. H. Eaves, Clark H. Lewis, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Comparison of wind tunnel and flight test measurements of static aerodynamic loading of a captive store /, also by R. E. Dix, G. R. Mattasits, 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: 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, Air Force Armament Laboratory (U.S.). sponsor, 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: 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, Air Force Armament Laboratory (U.S.). sponsor, 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: A Correlation of artifically induced boundary-layer transition data from blunt slender cones at hypersonic speeds /, also by A. H. Boudreau, 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: Dynamic stability characteristics of a 10-deg cone at Mach number 20 /, also by R. H. Urban, R. J. Shanahan, Aerospace Research Laboratories (U.S.). sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Effects of unit Reynolds number, nose bluntness, and roughness on boundary layer transition /, 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: Experimental Magnus and static stability characteristics of ballistic projectiles with various boattail angles and lengths at Mach numbers from 0.5 through 2.5 /, also by Leroy M. Jenke, T. O. Shadow, 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: An Experimental study of several wind tunnel wall configurations using two V/STOL model configurations /, also by T. 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: Force and pressure tests of two elliptic ogive body shapes at Mach numbers 5, 6, and 8 /, also by Jack L. Burk, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Forces and moments on base cover plates in the wake of a discoverer Mark 4 re-entry vehicle at transonic speeds /, also by H. L. Chevalier, P. D. Gerke, Arnold Engineering Development Center. issuing body, and United States. Air Force. Air Research and Development Command. sponsor (page images at HathiTrust)
• ARO, Inc. sponsor: A Generalized base-flow analysis with initial boundary-layer and chemistry effects /, also by John H. Fox, 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: Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /, also by W. T. Strike, S. Pate, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Investigation of drag reduction by boundary-layer suction on a body of revolution at Mach numbers 2.5, 3, and 3.5 /, also by S. R. Pate, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Investigation of suction controlled boundary layer on a Northrop model at Mach numbers of 2, 5, 3, and 3.5 /, also by W. T. Strike, J. C. Donaldson, and Arnold Engineering Development Center. issuing agency (page images at HathiTrust)
• ARO, Inc. sponsor: An investigation of the effects of shock impingement on a blunt leading edge /, also by A. D. Ray, R. L. Palko, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Measurement of the pressure flucuations in the test section of the 16-foot transonic circuit in the frequency range from 5 to 1000 CPS /, also by H. L. Chevalier, H. E. Todd, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: A Method for computing boundary-layer flows, including normal pressure gradient and longitudinal curvature effects /, also by Arloe W. Mayne, 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: A Method of calculating turbulent-boundary-layer growth at hypersonic Mach numbers /, also by James C. Sivells, Robert G. Payne, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: A Parametric investigation of the annular jet concept for obtaining afterbody drag data at transonic mach numbers /, also by Earl A. Price, 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: Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping /, also by W. N. MacDermott, Arnold Engineering Development Center. issuing body, and United States. Air Force. Air Research and Development Command. sponsor (page images at HathiTrust)
• ARO, Inc. sponsor: Pressure distribution tests of several sharp leading edge wings, bodies, and body-wing combinations at Mach 5 and 8 /, also by R. E. Randall, J. L. Burk, D. R. Bell, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Procedure used for X-15 heat transfer and pressure distribution tests at hypersonic speeds /, also by J. A. Durand, J. P. Rhudy, Arnold Engineering Development Center. issuing body, and United States. Air Force. Air Research and Development Command. sponsor (page images at HathiTrust)
• ARO, Inc. sponsor: Real-gas effects on the aerodynamics of blunt cones as measured in a hypervelocity range /, also by C. J. Welsh, 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: Real-gas laminar boundary layers in hypervelocity nozzles /, also by Willard E. Summers, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Results of 0.2-scale B-1 production inlet development and verification tests at subsonic and supersonic mach numbers /, also by R. F. Lauer, 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 full-scale B-1 inlet/engine compatibility test at subsonic and supersonic mach numbers /, also by H. E. McDill, 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: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies., also by John A. Benek, 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: Skin friction measurements at transonic mach numbers /, also by Charles L. Smith and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Sound and pressure measurements in cavities on a body of revolution at supersonic speeds /, also by J. C. Donaldson, D. R. Bell, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Static force and moment tests of the Holloman narrow-gage rocket sled at Mach Numbers from 1.5 to 4.0 /, also by R. H. Rhudy, J. D. Corce, 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: Tests of the Kaman KRC-6M rotochute at transonic speeds /, also by R. D. Herron, T. W. Binion, Kaman Aircraft Corporation. sponsor, United States. Air Force. Air Research and Development Command. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Unsteady transonic flow over blunt and pointed bodies of revolution /, also by Hsieh T., 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: The Use of boundary-layer suction for maintaining laminar flow downstream of a reflected incidence shock wave on a flat plate at free-stream Mach numbers 2.5, 3, and 3.5 /, also by S. R. Pate, Air Force Flight Dynamics Laboratory (U.S.). sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• ARO, Inc. sponsor: Vorticity-stream function formulation of compressible and incompressible turbulent internal flows /, also by John C. Chien, 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: Wind tunnel measurements of hysteresis in the static aerodynamic characteristics of aircraft /, also by J. F. Herman, 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: A Wind tunnel test to study the mutual interference of multiple bodies in the flow field of the F-4C aircraft in the transonic speed range /, also by A. A. Hesketh and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)

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