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United States. Air Force. Arnold Air Force Base

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• United States. Air Force. Arnold Air Force Base: The AEDC three-dimensional, potential flow computer program. Volume I. Method and computer program (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Donald C. Todd, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: The AEDC three-dimensional, potential flow computer program. Volume II. Mathematical modeling, application, and verification (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by Richard L. Palko, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Aerodynamic and cold jet plume geometry characteristics of the Army free rocket at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by E. S. Washington, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Aircraft motion sensitivity to dynamic stability derivatives (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by T. F. Langham, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Altitude-velocity table and charts for imperfect air. Volume I. Free-stream stagnation gas composition data (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Clark H. Lewis, E. G. Burgess, inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Steven F. Yaros, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Application of linearized transonic theory to tunnel blockage interference (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), also by C. F. Lo, United States. Air Force. Systems Command. Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Applications of the aerotherm BLIMP boundary-layer program to nonablating reentry flight conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by Emmett E. Edenfield, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Boundary-layer transition under hypersonic conditions (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. Leith Potter, Jack D. Whitfield, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Calculation of skin friction intwo-dimensional, transonic, turbulent flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by T. W. Swafford, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Captive trajectory system for AEDC supersonic wind tunnel (A) and hypersonic wind tunnels (B) and (C) (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), also by T. D. Buchanan, W. A. Crosby, Arnold Engineering Development Center, and Calspan Field Services (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Chimera : a grid-embedding technique (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1986., 1986), also by J. A. Benek, F. C. Dougherty, J. L. Steger, Ames Research Center, Calspan Corporation, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Combined effects of viscous interaction and ideal source flow on pressure and heat-transfer distributions over hemisphere cylinders at M infinity is approximately 18 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. H. Eaves, Clark H. Lewis, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Common geometry systems for the numerical representation of three-dimensional aerodynamic configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1984., 1984), also by K. Scott Keen, Arnold Engineering Development Center, and Calspan Field Services (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Comparison of wind tunnel and flight test measurements of static aerodynamic loading of a captive store (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1980., 1980), also by R. E. Dix, G. R. Mattasits, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume III. Appendixes F, Test number 6 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Inc ARO, Air Force Armament Laboratory (U.S.), and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings. Volume II. Appendixes A through E, Test numbers 1 through 5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), also by G. R. Gomillion, Inc ARO, Air Force Armament Laboratory (U.S.), and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Correlation of artifically induced boundary-layer transition data from blunt slender cones at hypersonic speeds (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by A. H. Boudreau, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Effects of unit Reynolds number, nose bluntness, and roughness on boundary layer transition (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1960., 1960), also by J. Leith Potter, Jack D. Whitfield, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An Evaluation of nozzle afterbody code : ARO2P (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1986., 1986), also by Frederick C. Guyton, Arnold Engineering Development Center, and Calspan Corporation (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Expansion of a jet into near vacuum (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Aerospace Environmental Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by R. A. Cassanova, W. B. Stephenson, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An Experimental investigation of techniques to suppress edgetones from perforated wind tunnel walls (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by N. Sam. Dougherty and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Experimental Magnus and static stability characteristics of ballistic projectiles with various boattail angles and lengths at Mach numbers from 0.5 through 2.5 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnell Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by Leroy M. Jenke, T. O. Shadow, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An Experimental study of several wind tunnel wall configurations using two V/STOL model configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by T. W. Binion, United States. Air Force. Systems Command. Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Flow generation properties of five transonic wind tunnel test section wall configurations (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. L. Parker and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Generalized base-flow analysis with initial boundary-layer and chemistry effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John H. Fox, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An Improved interaction method for calculating exhaust nozzle boattail flows (Mountain View, California : Nielsen Engineering & Research, Inc., 1980., 1980), also by Gary D. Kuhn, Arnold Engineering Development Center, and Nielsen Engineering & Research (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An investigation of the effects of shock impingement on a blunt leading edge (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by A. D. Ray, R. L. Palko, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: An Investigation of three-dimensional wall interference in a variable porosity transonice wind tunnel (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1974., 1974), also by Travis W. Binion, United States. Air Force. Systems Command. Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Method for computing boundary-layer flows, including normal pressure gradient and longitudinal curvature effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by Arloe W. Mayne, United States. Air Force. Systems Command. Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Method of calculating turbulent-boundary-layer growth at hypersonic Mach numbers (Arnold Air Force Base, Tennessee, Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by James C. Sivells, Robert G. Payne, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: A Parametric investigation of the annular jet concept for obtaining afterbody drag data at transonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Earl A. Price, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: PARC code : theory and usage (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), also by G. K. Cooper, J. R. Sirbaugh, Inc Sverdrup Technology, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: PARC code validation for propulsion flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1989., 1989), also by G. K. Cooper, W. J. Phares, G. D. Garrard, Arnold Engineering Development Center, and Inc Sverdrup Technology (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Real-gas effects on the aerodynamics of blunt cones as measured in a hypervelocity range (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by C. J. Welsh, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Real-gas laminar boundary layers in hypervelocity nozzles (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Willard E. Summers, Inc ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Real gas scale effects on hypersonic laminar boundary-layer parameters including effects of entropy-layer swallowing (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by J. C. Adams, E. O. Marchand, A. W. Mayne, W. R. Martindale, United States. Air Force. Systems Command. Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Results of 0.2-scale B-1 production inlet development and verification tests at subsonic and supersonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. F. Lauer, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Results of a full-scale B-1 inlet/engine compatibility test at subsonic and supersonic mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1975., 1975), also by H. E. McDill, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies. Part II. Detailed flow measurements (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by John A. Benek, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Static force and moment tests of the Holloman narrow-gage rocket sled at Mach Numbers from 1.5 to 4.0 (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1975., 1975), also by R. H. Rhudy, J. D. Corce, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Supersonic wind tunnel tests of the IDS 6208 rocket sled (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Von Kármán Gas Dynamics Facility, Air Force Systems Command, United States Air Force, 1965., 1965), also by Leroy M. Jenke, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Theoretical and experimental studies of hypersonic viscous effects (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1965., 1965), also by Clark H. Lewis, Jack D. Whitfield, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Unsteady transonic flow over blunt and pointed bodies of revolution (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), also by Hsieh T., Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Unsteady viscous-inviscid interaction procedures for transonic airfoil flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1984., 1984), also by Tracy Donegan, Arnold Engineering Development Center, and Calspan Field Services (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Vorticity-stream function formulation of compressible and incompressible turbulent internal flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1979., 1979), also by John C. Chien, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)
• United States. Air Force. Arnold Air Force Base: Wind tunnel measurements of hysteresis in the static aerodynamic characteristics of aircraft (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1979., 1979), also by J. F. Herman, Inc ARO, and United States. Air Force. Systems Command. Arnold Engineering Development Center (page images at HathiTrust)

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