Large scale hydrogen fueled supersonic combustor test at simulated Mach 8 flight, describing fuel injector design


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    Title :

    Large scale supersonic combustor testing at conditions simulating Mach 8 flight


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH ; 1970 ; SAN DIEGO, CA


    Publication date :

    1970-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English