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 prediction methods are suitable for use by design personnel during the preliminary design and evaluation of V/STOL aircraft of the type previously mentioned. The results of a literature survey are presented in this volume. (Author)


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    Title :

    V/STOL Aircraft Aerodynamic Prediction Methods Investigation. Volume IV. Literature Survey


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

    Publication date :

    1972


    Size :

    78 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English