Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6


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    Title :

    Flow phenomena and separation over highly swept delta wings with trailing-edge flaps at Mach 6.


    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


    Keywords :