This paper presents results for a single-pulse detonation tube wherein the effects of high temperature dissociation and the subsequent recombination influence the sensible heat release available for providing propulsive thrust. The study involved the use of ethylene and air at equivalence ratios of 0.7 and 1.0. The real gas effects on the sensible heat release were found to be significantly large so as to have an impact on the thrust, impulse and fuel consumption of a PDE.


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    Titel :

    Real Gas Effects on the Performance of Hydrocarbon-fueled Pulse Detonation Engines


    Beteiligte:

    Kongress:

    41st Aerospace Sciences Meeting ; 2003 ; Reno, NV, United States


    Erscheinungsdatum :

    01.03.2003


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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