Research programs at the NASA Langley Research Center on the development of airframe-integrated scramjet concepts (supersonic combustion ramjet) are reviewed briefly. The design and performance of a specific scramjet configuration are examined analytically by use of recently developed and substantiated techniques on boundary-layer development, heat transfer, fuel-air mixing, heat-release rates, and engine-cycle analysis. These studies indicate that the fixed-geometry scramjet module will provide practical levels of thrust performance with low cooling requirements. Areas which need particular emphasis in further development work are the combustor design for low speeds and the integrated nozzle design.


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    Titel :

    Design considerations for the airframe-integrated scramjet


    Beteiligte:
    Henry, J. R. (Autor:in) / Anderson, G. Y. (Autor:in)

    Kongress:

    Intern. Symp. on Air Breathing Engines ; 1972 ; Marseille, France


    Erscheinungsdatum :

    1973-12-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design Considerations for the Airframe-Integrated Scramjet

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    AIAA-2005-1280 AIRFRAME INTEGRATED SCRAMJET DESIGN AND PERFORMANCE ANALYSIS

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    Airframe/Scramjet Integrated Design of Hypersonic Cruise Vehicle AIAA Paper

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