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United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body

Books from the extended shelves:

• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: The AEDC three-dimensional, potential flow computer program., also by Donald C. Todd, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: The AEDC three-dimensional, potential flow computer program., also by Richard L. Palko, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Aerodynamic and cold jet plume geometry characteristics of the Army free rocket at transonic mach numbers /, also by E. S. Washington, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc.. sponsor ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Aircraft motion sensitivity to dynamic stability derivatives /, also by T. F. Langham, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes /, also by Steven F. Yaros, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Application of linearized transonic theory to tunnel blockage interference /, also by C. F. Lo, United States. Air Force. Arnold Air Force Base. sponsor, and Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Applications of the aerotherm BLIMP boundary-layer program to nonablating reentry flight conditions /, also by Emmett E. Edenfield, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Calculation of skin friction intwo-dimensional, transonic, turbulent flow /, also by T. W. Swafford, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: CFD wing/pylon/finned store mutual interference wind tunnel experiment /, also by E. Rolland Heim and Calspan Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Comparison of wind tunnel and flight test measurements of static aerodynamic loading of a captive store /, also by R. E. Dix, G. R. Mattasits, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings., also by G. R. Gomillion, Inc. sponsor ARO, Air Force Armament Laboratory (U.S.). sponsor, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings., also by G. R. Gomillion, Inc. sponsor ARO, Air Force Armament Laboratory (U.S.). sponsor, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: A Correlation of artifically induced boundary-layer transition data from blunt slender cones at hypersonic speeds /, also by A. H. Boudreau, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Documentation of the Phase III 0.192-scale Northrop/McDonnell-Douglas F-18 inlet performance test at mach numbers 0 to 1.55 /, also by Jimmy Walker, Sverdrup Corporation. sponsor, and United States. Naval Air Systems Command. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: An Experimental investigation of techniques to suppress edgetones from perforated wind tunnel walls /, also by N. Sam. Dougherty and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc. sponsor ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Flow generation properties of five transonic wind tunnel test section wall configurations /, also by R. L. Parker and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: A Generalized base-flow analysis with initial boundary-layer and chemistry effects /, also by John H. Fox, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: An Investigation of the effects of nose geometry on the aerodynamic characteristics of a full scale vertical launch ASROC forebody at M₀₀ = 0.30 /, also by R. M. Vaeth, Calspan Corporation. sponsor, and Naval Ocean Systems Center (U.S.). sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc. sponsor ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: A Parametric investigation of the annular jet concept for obtaining afterbody drag data at transonic mach numbers /, also by Earl A. Price, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Pressure and static force test of three elliptic missile body configurations at mach numbers 1.5 to 5.0 /, also by M. E. Sellers, L Siler, Air Force Wright Aeronautical Laboratories. sponsor, and Calspan Field Services. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Pressure test of three elliptic missile body configuratins /, also by Marvin E. Sellers and Calspan Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Real-gas effects on the aerodynamics of blunt cones as measured in a hypervelocity range /, also by C. J. Welsh, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc. ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Results of 0.2-scale B-1 production inlet development and verification tests at subsonic and supersonic mach numbers /, also by R. F. Lauer, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Results of a full-scale B-1 inlet/engine compatibility test at subsonic and supersonic mach numbers /, also by H. E. McDill, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies., also by John A. Benek, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Skin friction measurements at transonic mach numbers /, also by Charles L. Smith and Inc.. sponsor ARO (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Static force and moment test of the Holloman narrow-gage rocket slet at Mach numbers from 3.5 to 5.5 /, also by C. L. Ratliff and Calspan Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Static stability test of three elliptic missile body configurations /, also by Marvin E. Sellers and Calspan Corporation. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Unsteady transonic flow over blunt and pointed bodies of revolution /, also by Hsieh T., Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Vorticity-stream function formulation of compressible and incompressible turbulent internal flows /, also by John C. Chien, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: Wind tunnel measurements of hysteresis in the static aerodynamic characteristics of aircraft /, also by J. F. Herman, Inc. sponsor ARO, and United States. Air Force. Arnold Air Force Base. sponsor (page images at HathiTrust)
• United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body: 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 Inc.. sponsor ARO (page images at HathiTrust)

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Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
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