Analytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The aircraft configurations studies have a conventional wing, fuselage and empennage. The prediction methods are suitable for use by design personnel during the preliminary design and evaluation of V/STOL aircraft of the type previously mentioned. Details and listings of the computer programs associated with the prediction methods are given in the volume. (Author)


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    Titel :

    V/STOL Aircraft Aerodynamic Prediction Methods Investigation. Volume III. Manual for Computer Programs


    Beteiligte:
    P. T. Wooler (Autor:in) / H. C. Kao (Autor:in) / M. F. Schwendemann (Autor:in) / H. R. Wasson (Autor:in) / H. Ziegler (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    205 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch