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    Title :

    An Integrated Aeroramp-Injector/Plasma Igniter for Hydrocarbon Fuels in Supersonic Flow - Part A: Experimental Studies of the Geometric Configuration



    Conference:

    International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan



    Publication date :

    2001-01-01


    Size :

    13 pages


    Remarks:

    Contains papers AIAA-2001-1750 to 1927 only with gaps



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English







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