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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    Title :

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


    Contributors:

    Publication date :

    1977


    Size :

    162 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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