F-111A airplane in-flight inlet pressure fluctuations for engine compressor surge, discussing average turbulence factor


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    Title :

    Analysis of in-flight pressure fluctuations leading to engine compressor surge in an F-111A airplane for Mach numbers to 2.17


    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


    Keywords :