The drag coefficients of several bodies of revolution which are significant for the purpose of aerodynamic deceleration were measured in the transonic flow regime and at supersonic speeds of Mach numbers 4 and 5. (Author)


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    Title :

    Drag Coefficients of Several Bodies of Revolution at Transonic and Supersonic Velocity


    Contributors:
    H. G. Heinrich (author) / S. R. Hess (author) / G. Stumbris (author)

    Publication date :

    1964


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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