Titlebook: Supercritical Wing Sections III; Frances Bauer,Paul Garabedian,David Korn Book 1977 Springer-Verlag Berlin Heidelberg 1977 design.developm

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Plots and Tables of Results,Below we present several airfoils that were designed by use of the new code K.

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Book 1977Aeronautics and Space Administration at the Energy Research and Development Administration Mathematics and Computing Laboratory of New York University. The work was performed under NASA Grants NGR 33-016-167 and NGR 33-016-201 and ERDA Contract EY-76-C-02-3077. Computer programs to be listed and des

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The Method of Complex Characteristics,graph plane corresponds to points in the complex domain where ξ. = η?.. To calculate φ and ψ paths of integration are laid down in the complex plane, and then a stable finite difference scheme is applied to solve the characteristic initial value problem (see Volume I).

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Introduction,has played a central role in the development of new supercritical wing sections. One of the principal tools is a fast and reliable code that simulates two-dimensional wind tunnel data for transonic flow at high Reynolds numbers (see Volume II). This is used widely by industry to assess drag creep an

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The Method of Complex Characteristics,m function that presuppose conservation of entropy. In terms of characteristic coordinates ξ and η we have . The coordinates ξ and n can be specified in terms of the speed q and the flow angle θ by the formulas . where f is any complex analytic function. Prescription of a second arbitrary function g

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