Real air hypersonic shock-heated flow parameters at high speeds and high altitudes


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    Title :

    Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet


    Contributors:

    Publication date :

    1963-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English