Shock tube technique for producing subsonic, transonic and supersonic flows with high Reynolds numbers


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    Title :

    A shock tube technique for producing subsonic, transonic, and supersonic flows with extremely high Reynolds numbers.


    Contributors:

    Conference:

    AEROSPACE SCIENCES MEETING ; 1968 ; NEW YORK, NY


    Publication date :

    1968-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English