This paper presents performance results for pulse detonation engines (PDE) taking into account the effects of dissociation and recombination. The amount of sensible heat recovered through recombination in the PDE chamber and exhaust process was found to be significant. These results have an impact on the specific thrust, impulse and fuel consumption of the PDE.


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    Title :

    Airbreathing Pulse Detonation Engine Performance


    Contributors:

    Conference:

    Combustion, Airbreathing Propulsion, Propulsion Systems Hazards, and Modelling and Simulation Subcommittees Joint Meeting


    Publication date :

    2002-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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