Variable geometry supersonic aircraft design, discussing inlet and exhaust nozzles problems and wind tunnel tests


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    Title :

    Variable geometry requirements in inlets and exhaust nozzles for high Mach number applications.


    Contributors:

    Conference:

    INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES, CONGRESS ; 1968 ; MUNICH, GERMANY


    Publication date :

    1968-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :