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    Title :

    Reynolds number and cowl position effects for a generic sidewall compression scramjet inlet at Mach 10 - A computational and experimentalinvestigation


    Contributors:

    Conference:

    17th Aerospace Ground Testing Conference ; 1992 ; Nashville , TN , U.S.A.



    Publication date :

    1992-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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