Studies on the effects of a subsonic flight environment on fuels refined for high Mach number application are reported. Requirements and hydrocarbon composition for fuel to withstand high Mach number stresses are cited and their compatibility with conventional systems at low temperatures is discussed.


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    Titel :

    High Temperature Hydrocarbon Fuels and Subsonic Flight Environments


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hager, John A. (Autor:in)

    Kongress:

    1965 International Automotive Engineering Congress and Exposition ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High temperature hydrocarbon fuels and subsonic flight environments

    Hager, J.A. | Engineering Index Backfile | 1965


    Flight research at high subsonic speeds

    Davies, H. | Engineering Index Backfile | 1948


    Flight Demonstration of the High Burning Rate Hydrocarbon-Based Hybrid Rocket Fuels

    Karabeyoglu, Arif / Zilliac, Greg / Castellucci, Paul et al. | AIAA | 2003


    Jet shock noise at high subsonic flight

    Wat, J. / Yamamoto, K. / Golub, R. | AIAA | 2000


    Flight effects on subsonic jet noise

    SAROHIA, V. | AIAA | 1979