Airframe installation effects at transonic speeds on underwing supersonic cruise exhaust nozzles, using flight and wind tunnel tests


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    Title :

    Flight and wind tunnel investigation of installation effects on underwing supersonic cruise exhaust nozzles at transonic speeds


    Contributors:

    Conference:

    NATO, AGARD, AERODYNAMIC INTERFERENCE SPECIALISTS MEETING ; 1970 ; SILVER SPRING, MD


    Publication date :

    1970-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :