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    Title :

    Shock interaction effect on a flapped delta wing at M equals 8.2


    Author / Creator :

    RAO, D. M. /NASA, LANGLEY RESEARCH CENTER, HYPERSONIC VEHICLES DIV.,HAMPTON, VA./.


    Contributors:
    RAO, D. M. (author)

    Published in:

    AIAA Journal ; 9 , 5 ; 985-986


    Publication date :

    1971-01-01


    Size :

    2 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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