This viewgraph representation provides an overview of research which develops a quasi one dimensional chemistry computational fluid dynamics code to study the effect of nozzle design on the performance of pulse detonation rocket engines (PDREs). Topics considered include: PDREs vs. steady-state rocket engines (SSREs), PDRE cycles, numerical models of idealized PDRE performance, thrust determination of PDRE, specific geometries, and nozzle design and geometry.


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    Title :

    Quasi 1-D Study of Pulse Detonation Rocket Engine Blowdown Gasdynamics and Performance


    Contributors:

    Conference:

    Propulsion Engineering Research Center 14th Annual Symposium on Propulsion ; 2002 ; State College, PA, United States


    Publication date :

    2002-12-02


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English








    Simplified Analysis of Pulse Detonation Rocket Engine Blowdown Gasdynamics and Performance

    Morris, C. I. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 2002