Aerodynamic characteristics at Mach numbers 1.60 to 2.16 of blunt-nose missile model having triangular cross section and fixed triform fins


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    Title :

    Aerodynamic characteristics at Mach numbers from 1.60 to 2.16 of a blunt-nose missile model having a triangular cross section and fixed triform fins


    Contributors:

    Publication date :

    1971-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :