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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:
    P. T. Wooler (author) / H. C. Kao (author) / M. F. Schwendemann (author) / H. R. Wasson (author) / H. Ziegler (author)

    Publication date :

    1972


    Size :

    205 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English