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    Titel :

    Evaluation of a High Bypass Turbofan Hybrid Utilizing a Pulsed Detonation Combustor


    Beteiligte:
    Andrus, Ionio (Autor:in) / King, Paul (Autor:in)

    Kongress:

    43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit



    Erscheinungsdatum :

    2007-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Evaluation of a High Bypass Turbofan Hybrid Utilizing a Pulsed Detonation Combustor AIAA Paper

    Andrus, I. / King, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007


    Experimental Investigations of a Pulsed Detonation Combustor-Turbine Hybrid System

    Deng, Jun-xiang / Zheng, Long-xi / Yan, Chuan-jun et al. | AIAA | 2009


    Experimental Investigations of a Pulsed Detonation Combustor-Turbine Hybrid System

    Deng, J. / Zheng, L. / Yan, C. et al. | British Library Conference Proceedings | 2009


    Propulsion Simulator for High Bypass Turbofan Performance Evaluation

    Balan, Chellappa / Hoff, Gregory E. | SAE Technical Papers | 1993


    Wave Attenuation and Interactions in a Pulsed Detonation Combustor-Turbine Hybrid System

    Rasheed, Adam / Furman, Anthony / Dean, Anthony | AIAA | 2006