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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    Titel :

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


    Beteiligte:
    W. J. Runciman (Autor:in) / G. R. Letsinger (Autor:in) / B. F. Ray (Autor:in) / F. W. May (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    234 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch