Jet engine compressor stalls in-flight investigation up to Mach 2 on F-111A by pressure sensors, noting steady state distortion role


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    Title :

    The flight investigation of pressure phenomena in the air intake of an F-111A airplane.


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.


    Publication date :

    1969-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English