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  • 1970-1974  (2)
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  • 1
    facet.materialart.
    Unknown
    Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The configuration and performance of the propulsion system for the hypersonic research vehicle are discussed. A study of the interactions between propulsion and aerodynamics of the highly integrated vehicle was conducted. The hypersonic research vehicle is configured to test the technology of structural and thermal protection systems concepts and the operation of the propulsion system under true flight conditions for most of the hypersonic flight regime. The subjects considered are: (1) research vehicle and scramjet engine configurations to determine fundamental engine sizing constraints, (2) analytical methods for computing airframe and propulsion system components, and (3) characteristics of a candidate nozzle to investigate vehicle stability and acceleration performance.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-TM-X-71972
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Studies of engine-airframe integration on hypersonic aircraft (1970)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Airframe-propulsion system integration for Mach 6 transport and Mach 12 research airplane, examining off-design operation effects and interaction of aerodynamic forces
    Keywords: AIRCRAFT
    Type: AIAA PAPER 70-542 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ATMOSPHERIC FLIGHT MECHANICS CONFERENCE; May 13, 1970 - May 15, 1970; TULLAHOMA, TN
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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