In this paper, the effect of flight Mach number on the relative performance of pulse detonation engines and gas turbine engines is investigated. The effect of ram and mechanical compression on combustion inlet temperature and the subsequent sensible heat release is determined. Comparison of specific thrust, fuel consumption and impulse for the two engines show the relative benefits over the Mach number range.


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    Titel :

    Role of Air-Breathing Pulse Detonation Engines in High Speed Propulsion


    Beteiligte:
    L. A. Povinelli (Autor:in) / J. H. Lee (Autor:in) / M. O. Anderberg (Autor:in)

    Erscheinungsdatum :

    2001


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Role of Air-Breathing Pulse Detonation Engines in High Speed Propulsion

    Povinelli, Louis A. / Lee, Jin-Ho / Anderberg, Michael O. | NTRS | 2001





    Pulse Detonation Engines for High Speed Flight

    Povinelli, Louis A. | NTRS | 2002