Equations for intermediate range missile, presented in form suitable for application of differential analyzer and digital computer techniques, provide description of mo tion of aerodynamically controlled winged vehicles and are applicable to terminal accuracy and dynamic stability studies where higher order effects are of interest.


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    Title :

    General air-frame dynamics of guided missile


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Byrum, B.L. (author) / Grady, E.R. (author)


    Publication date :

    1955


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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