The report presents methods for predicting the performance determining aerodynamic characteristics and the stability derivatives of transport-type configurations employing the vectored-thrust mechanical-flap high-lift concept. These methods are suitable for preliminary design. They have been automated in a FORTRAN 4 computer program, for which a users' manual and listing are included in this document. (Author)


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    Title :

    STOL Tactical Aircraft Investigation. Volume II. Part I. Aerodynamic Technology: Design Compendium, Vectored Thrust/Mechanical Flaps


    Contributors:
    W. J. Runciman (author) / G. R. Letsinger (author) / B. F. Ray (author) / F. W. May (author)

    Publication date :

    1973


    Size :

    234 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English