Method based on superposition of results of potential theory and viscous force on cylindrical body due to transverse component of flow; application to aerodynamic design of aircraft rockets.


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    Title :

    Estimation of normal-force, drag, and pitching-moment coefficients for blunt-based bodies of revolution at large angles of attack


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Kelly, H.R. (author)


    Publication date :

    1954


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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