The Online Books Page

Scale models

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• Supersonic aerodynamic characteristics of a 1/6-scale model of the final two stages of the Argo D-4 four-stage rocket vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1965), by Clyde Hayes, William A. Corlett, and Langley Research Center (page images at HathiTrust)
• Aerodynamic characteristics of 0.187-scale model of a target missile at Mach 1.80 to 2.16 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by William A. Corlett and Langley Research Center (page images at HathiTrust)
• Aerodynamic and acoustic tests of duct-burning turbofan exhaust nozzles / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1976), by Hilary Kozlowski, Allan B. Packman, Langley Research Center, and Pratt & Whitney Aircraft Company (page images at HathiTrust)
• Aerodynamic characteristics of a 0.0667-scale model of the X-15A-2 research airplane at transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by James C. Patterson and Langley Research Center (page images at HathiTrust)
• Model tests of jet-induced lift effects on a VTOL aircraft in hover / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by P. K. Shumpert, J. G. Tibbetts, Langley Research Center, Lockheed-Georgia Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic characteristics, temperature, and noise measurements of a large-scale external-flow jet-augmented-flap model with turbojet engines operating / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Marvin P. Fink, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Rapid-transition tests of a 1/4-scale model of the VZ-2 tilt-wing aircraft / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Louis P. Tosti, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Low-speed wind-tunnel investigation of a wingless jet VTOL transport model / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Marion O. McKinney and Langley Research Center (page images at HathiTrust)
• A study of methods for simulating the atmosphere entry of vehicles with small-scale models / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Byron L. Swenson and Ames Research Center (page images at HathiTrust)
• Effect of chordwise heat conduction on the torsional stiffness of a diamond-shaped wing subjected to a constant heat input / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Robert G. Thomson, J. Lyell Sanders, and Langley Research Center (page images at HathiTrust)
• Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Ross B. Robinson and Langley Research Center (page images at HathiTrust)
• Rear end structural crashworthiness of perimeter frame vehicles, design development and verification. Final report. (1972), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
• Rear end structural crashworthiness of perimeter frame vehicles. Summary report. Final report. (1972), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
• An experimental study of highway aerodynamic interferences. Final report. (1978), by D. P. Telionis, C. J. Fahrner, and G. S. Jones (page images at HathiTrust)
• Photogrammetric dimensioning of ships' engine-room models. (1981), by John F. Kenefick and L. D. Chirillo (page images at HathiTrust; US access only)
• Rear end structural crashworthiness of unitized construction vehicles, design development and design verification. Final report. (1973), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
• Rear end structural crashworthiness of unitized construction vehicles - summary report. Final report. (1973), by Robert L. Anderson and E. Enserink (page images at HathiTrust)
• Methods, application and cost effectiveness of scale model studies of automobile impacts. Final report. (1974), by B. S. Holmes, G. E. Sliter, and H. E. Lindberg (page images at HathiTrust)
• Research safety vehicle - phase II. Volume IIIb: subcontractor final reports. (1977) (page images at HathiTrust)
• Scale model study of low-density concrete impact attenuators. Final report. (1978), by Jack D. Bakos (page images at HathiTrust)
• Development and experimental evaluation of a steel tube vehicle impact attenuation system. Final report. (1981), by John F. Carney (page images at HathiTrust)
• Use of scale models as a management tool. (1974) (page images at HathiTrust; US access only)
• Cleveland Harbor, Ohio, design for the safe and efficient passage of 1,000-ft-long vessels at the west (main) entrance: hydraulic model investigation. Final report. (1983), by Robert R. Bottin (page images at HathiTrust; US access only)

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