Box 2
Contains 27 Results:
Printed Material, 1953 - 1986
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
National Advisory Committee for Aeronautics, Ames Research Center. Equations, Tables, and Charts for Compressible Flow. Washington, DC: Government Printing Office, 1953
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Schaefer, W. T. Jr. Characteristics of Major Active Wind Tunnels at the Langley Research Center. NASA TM X-1130. Washington, DC: National Aeronautics and Space Administration, 1965
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Historical Aspects of NASA Scramjet Technology Development, by E. A. Mackley, circa early 1970s
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Hypersonic Research Facilities Study, Volume I, Summary, prepared under Contract No. NAS2-5458 by Advanced Engineering at McDonnell Aircraft Company for OART – Advanced Concepts and Missions Division, NASA, Moffett Field, California, October 1970
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Hunt, J. L.; Talcott, N. A. Jr.; Cubbage, J. M. Scramjet Exhaust Simulation Technique for Hypersonic Aircraft Nozzle Design and Aerodynamic Tests. Hampton, Virginia: NASA Langley Research Center, 1977
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr. Thermodynamic Properties of Gaseous Fluorocarbons and Isentropic Equilibrium Expansions on Two Binary Mixtures of Fluorocarbons and Argon. NASA TN D-8405. Washington, DC: National Aeronautics and Space Administration, 1977
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Draper, A. C.; Lane, P. Jr.; Zima, W. P. A Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology. Wright-Patterson Air Force Base, OH: Air Force Flight Dynamics Laboratory. (printed in AIAA 1977 AFM Conference, August 8 - 10, 1977
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr.; Hunt, J. L. Streamtube Analysis of a Hydrogen-Burning Scramjet Exhaust and Simulation Technique. Reprinted from Journal of Aircraft, Vol. 14, No. 9, September 1977, pp. 918-920, September 1977
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr.; Hunt, J. L. Calculated Heating on the Afterbody Nozzle of a Hypersonic Aircraft Concept. Reprinted from Journal of Aircraft, Vol. 14, No. 12, December 1977, pp. 1247-1248, September 1977
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr. Flow Field Visualization About External Axial Corners. NASA TM-78682. Hampton, Virginia: NASA Langley Research Center, 1978
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Weidner, J. P. The Application of Dual Fuel (JP-LH2) for Hypersonic Cruise Vehicles. Reprinted from Journal of Aircraft, Vol. 15, October, pp. 686-691, 1978
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Weidner, J. P. Conceptual Study of a Turbojet/Ramjet Inlet. NASA TM-80141. NASA Scientific and Technical Branch, 1979
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Beach, H. L. Jr. Hypersonic Propulsion, NASA Conference Publication 2092, Aeropropulsion 1979, Proceedings of a Conference held at NASA Lewis Research Center, Cleveland, Ohio, May 15 - 16, 1979
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Small, W. J.; Riebe, G. D.; Taylor, A. H. Aerodynamics of a Turbojet-Boosted Launch Vehicle Concept, presented at the AIAA 18th Aerospace Science Meeting, Pasadena, CA, January 14 - 16, 1980
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Weidner, J. P. Propulsions/Airframe Integration Considerations for High Altitude Hypersonic Cruise Vehicles, presented at the AIAA 18th Aerospace Sciences Meeting, Pasadena, CA, January 14 - 16, 1980
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Vahl, W. A.; Weidner, J. P. A Preliminary Assessment of the Impact of 2-D Exhaust-Nozzle Geometry on the Cruise Range of a Hypersonic Aircraft With Top-Mounted Ramjet Propulsion. NASA TM -81841. NASA Scientific and Technical Information Branch, 1980
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Pittman, J. L.; Riebe, G. D. Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2.96, 3.96, and 4.63. NASA TP-1767, NASA Scientific and Technical Information Branch, December 1980
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr. The Use of Interactive Graphic Displays for Interpretation of Surface Design Parameters. NASA Technical Memorandum 81963. NASA Scientific and Technical Information Branch, May 1981
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Rieble, G. D.; Small, W. J.; Morris, O. A. Aerodynamic Tests and Analysis of a Turbojet-Boosted Launch Vehicle Concept (Spacejet) Over a Mach Number Range of 1.50 to 2.86. NASA Technical Paper 1888. NASA Technical Memorandum 81963. NASA Scientific and Technical Information Branch, July 1981
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Heldenfels, R. R. Some Historical Perspectives on Thermostructural Research at the NACA Langley Aeronautical Laboratory, 1948-1958, presented at Symposium on Computational Aspects of Heat Transfer in Structures, Langley Research Center, Hampton, Virginia, November 3 - 5, 1981
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Talcott, N. A. Jr. Computer Graphics Display Technique for the Examination of Aircraft Design Data. Reprinted from Journal of Aircraft, Volume 19, Number 1, pp. 76-80, January 1982
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Hunt, J. L.; Johnston, P. J.; Cubbage, J. M., et. al. Hypersonic Airbreathing Missile Concepts Under Study at NASA Langley Research Center. AIAA 20th Aerospace Sciences Meeting, Orlando, Florida, January 11 - 14, 1982
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Wieting, A. R. Modification of 8 Foot High Temperature Tunnel to Provide a Unique National Research Facility for Hypersonic Air-Breathing Propulsion Systems, Proposed LaRC FY 85 CoF, September 1982
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”
Material and Structural Aspects of Lifting Re-Entry Aerospace Flight Systems, PowerPoint presentation sheets, no author, circa 1982
The printed material consists of a 1953 National Advisory Committee for Aeronautics document with equations, tables, and charts for compressible flow. Also included is a collection of research related to wind tunnels, Scramjet technology, hypersonic aircraft, and a paper titled, Flight Research Vehicle to Bridge Shuttle and Hypersonic Aircraft Technology.”