A quadrature method is derived for calculating the incompressible-flow aerodynamics of arbitrarily cambered jet-flapped airfoils. The anticipated application of the methodology is to high-speed subsonic flows (combat maneuvering aircraft) via the use of compressible-flow similarity transformations. The method yields the aerodynamic properties in terms of integrals having integrands which consist of the product of the camber-line ordinate and an influence function which is a parametric function of the jet-momentum coefficient. In general, the integrals involved must be evaluated by numerical methods. Tables of the necessary influence functions are given in the report.


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    Titel :

    Cambered Jet-Flapped Airfoil Theory with Tables and Computer Programs for Application


    Beteiligte:
    H. W. Woolard (Autor:in) / B. F. Niehaus (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    162 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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