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Wind tunnel models

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• Models and modelmaking
• Wind tunnels

• Wind tunnel models -- Bibliography
• Wind tunnel models -- Materials
• Wind tunnel models -- Testing

• Wind tunnels -- Models

• Wind tunnel modeling of flow and diffusion over San Nicolas Island, California (Pacific Missile Range, 1967), by Robert N Meroney and J. E. Cermak (page images at HathiTrust)
• Sand transport by wind (National Science Foundation, 1966), by T. Y Chiu (page images at HathiTrust)
• Comparison of full-scale and model buffet response of Apollo boilerplate service module (National Aeronautics and Space Administration ;, 1966), by Robert V. Doggett and Langley Research Center (page images at HathiTrust)
• Experimental evaluation of two turning vane designs for high-speed corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Royce D. Moore, Rickey J. Shyne, Donald R. Boldman, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of Reynolds number and model support on the supersonic aerodynamic chacteristics of a 140° included-angle cone (National Aeronautics and Space Administration ;, 1974), by Charles D. Trescot, Dorothy T. Howell, Clarence A. Brown, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of an advanced general aviation canard configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Joseph R. Chambers, Thomas M. Moul, Long P. Yip, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Michael J. See, James V. Cozzolongo, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Influence of upstream flow discontinuities on the acoustic power radiated by a model air jet (National Aeronautics and Space Administration ;, 1967), by Colin G. Gordon, Gideon Maidanik, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A wind model for an elevated stol-port configuration (National Aeronautics and Space Administration, 1974), by J. A. Peterka, J. E. Cermak, Ames Research Center, and Colorado State University (page images at HathiTrust)
• Subsonic and supersonic static aerodynamic characteristics of a family of bulbous base cones measured with a magnetic suspension and balance system (National Aeronautics and Space Administration ;, 1972), by Milan Vlajinac, Langley Research Center, and Massachusetts Institute of Technology (page images at HathiTrust)
• Correlation of sonic-boom theory with wind-tunnel and flight measurements (National Aeronautics and Space Administration, 1964), by Harry W. Carlson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
• Investigation of flow-field development for a series of sonic-boom wind-tunnel models (National Aeronautics and Space Administration ;, 1971), by Harry L. Runyan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of the low-speed high-lift aerodynamics of a one-fifth scale variable-sweep supersonic transport (National Aeronautics and Space Administration, 1968), by Anthony M. Cook, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of hinge moments for a simple delta wing and a delta-wing orbiter concept at mach 6 (National Aeronautics and Space Administration, 1972), by George C. Ashby, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds (National Aeronautics and Space Administration, 1960), by Mary W. Jackson, K. R. Czarnecki, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6 (National Aeronautics and Space Administration :, 1971), by Walter P. Nelms, Charles L. Thomas, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exploratory investigation of a transport configuration designed for supersonic cruise flight near a Mach number of 3 (National Aeronautics and Space Administration, 1960), by Ausley B. Carraway, Melvin M. Carmel, Donald T. Gregory, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6416 (National Aeronautics and Space Administration ;, 1971), by Harry H. Heyson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of the aerodynamic characteristics of a model representative of a supersonic fighter-class airplane with an external-flow jet-augmented flap in low-speed flight (National Aeronautics and Space Administration, 1959), by William A. Newsom and Langley Research Center (page images at HathiTrust)
• A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen (National Aeronautics and Space Administration, 1959), by Samuel Stein and Langley Research Center (page images at HathiTrust)
• Investigation of double slotted flaps on a swept-wing transport model (National Aeronautics and Space Administration, 1959), by Rodger L. Naeseth, Edwin E. Davenport, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of steady-state aerodynamics of a composite-lift VTOL aircraft model (National Aeronautics and Space Administration ;, 1969), by Matthew M. Winston, Robert J. Huston, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Use of hexafluoroethane to simulate the inviscid real-gas effects on blunt entry vehicles (National Aeronautics and Space Administration ;, 1974), by James L. Hunt, Kathryn A. Smith, Robert A. Jones, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration (National Aeronautics and Space Administration ;, 1975), by Arthur E. Phelps and Langley Research Center (page images at HathiTrust)
• Micrometeorological wind tunnel facility : description and characteristics (Fluid Dynamics and Diffusion Laboratory, Colorado State University, 1963), by Erich J. Plate, J. E. Cermak, and Colorado State University. Fluid Dynamics and Diffusion Laboratory (page images at HathiTrust; US access only)
• ALMR MOD A RVACS sensitivity to wind effects via wind tunnel modeling (Argonne, Illinois : Argonne National Laboratory, Reactor Engineering Division, 1993., 1993), by B. Bonomo, W. H. Gunther, University of Chicago, and Argonne National Laboratory (page images at HathiTrust)
• Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics (U.S. G.P.O., 1925), by Max M. Munk and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• the Joint NOL/RAE/WRE research program on bomb design : part 4 - the exterior ballistics of bomb design (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Frank J. Regan, F. J. Tanner, J. H. Shannon, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Self-compensating store ejection. (Silver Spring, Maryland : Naval Ordnance Laboratory, 1974., 1974), by Raymond R. Maestri, Leon H. Schindel, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Experimental study of forces and moments on circular bodies at high angle of attack (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Jr. Wardlaw and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume III, Additional data for two-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 2, Additional data for the one-jet configuration (Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by C. F. Ehrlich, C. M. Onspaugh, R. S. Peyton, J. J. Rising, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), by F. L. Guard, H. D. Schultz, Air Force Flight Dynamics Laboratory (U.S.), and Lockheed-California Company (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Aerodynamic stability and control/wind tunnel data correlation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by G. R. Casteel, Air Force Flight Dynamics Laboratory (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 4, Additional data for three-jet configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 1, Test description and data analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Sting dynamics of wind tunnel models (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), by James P. Billingsley, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Wind tunnel investigation of a spike-bluff body combination for a monorail rocket sled M = 2.0 to M = 5.0 (Holloman Air Force Base, New Mexico : Air Force Office of Scientific Research, Directorate of Research Analyses, United States Air Force, 1962., 1962), by Rudolf Hermann, Donald Olson, Frederick Moynihan, United States. Air Force. Office of Scientific Research, Rosemount Aeronautical Laboratories, and University of Minnesota. Institute of Technology (page images at HathiTrust)
• Strength evaluation of socket joints (National Aeronautics and Space Administration, Langley Research Center, 1994), by Larry C. Rash and Langley Research Center (page images at HathiTrust)
• A laboratory investigation into flight path perturbations during steep descents of V/STOL aircraft (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1976), by L. D. Reid, Peter C. Hughes, H. W. Teunissen, Bernard Etkin, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)

• Support interference of wind tunnel models : a selective annotated bibliography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by Marie H. Tuttle, Pierce L. Lawing, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models (National Aeronautics and Space Administration ;, 1974), by Richard F. Romanowski, Ira H. Steinberg, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)

• Force measurements on axisymmetric models with hammerhead noses at transonic speeds (National Aeronautics and Space Administration, 1967), by Bruno J. Gambucci, Robert C. Robinson, and Ames Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Making and collecting military miniatures. (R. M. McBride Co., 1957), by Bob Bard (page images at HathiTrust; US access only)
• Modelmaking for industrial design. (McGraw-Hill, 1958), by Ralph R. Knoblaugh (page images at HathiTrust)
• The construction of models for protective concealment. (Fort Belvoir, Va., 1942), by United States Army Corps of Engineers (page images at HathiTrust)
• The draftsman (The Scientific publishing bureau, 1919), by Robert Warren Shelmire (page images at HathiTrust)
• The art of working in pasteboard : upon scientific principles, to which is added, an appendix, containing directions for constructing architectural models, intended as a sequel to Papyro-plastics, or The art of modelling in paper : manual (Boosey & Sons, 1827), by Bernard Heinrich Blasche and D. Boileau (page images at HathiTrust)
• Papyro-plastics, or The art of modelling in paper; being an instructive amusement for persons of both sexes. From the German (Printed for Boosey and Sons, 1825), by Bernard Heinrich Blasche and D. Boileau (page images at HathiTrust)
• Papparbeiter (In der Buchhandlung der Erziehungsanstalt, 1805), by Bernhard Heinrich Blasche (page images at HathiTrust)
• Ohio River cooling water study (Argonne National Laboratory, 1974), by Brian P. Butz (page images at HathiTrust; US access only)
• The modelmaker: for those interested in making working models. (New York : Spon & Chamberlain, 1924-, 1924), by Spon & Chamberlain (page images at HathiTrust)
• Annotated bibliography on simulation in the social sciences (Department of Sociology and Anthropology, Iowa Agricultural and Home Economics Experiment Station, Iowa State University, 1966), by John J. Hartman (page images at HathiTrust; US access only)

More items available under broader and related terms at left.