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    A general panel method for the analysis and design of arbitrary configurations in incompressible flows (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A method for solving the linear integral equations of incompressible potential flow in three dimensions is presented. Both analysis (Neumann) and design (Dirichlet) boundary conditions are treated in a unified approach to the general flow problem. The method is an influence coefficient scheme which employs source and doublet panels as boundary surfaces. Curved panels possessing singularity strengths, which vary as polynomials are used, and all influence coefficients are derived in closed form. These and other features combine to produce an efficient scheme which is not only versatile but eminently suited to the practical realities of a user-oriented environment. A wide variety of numerical results demonstrating the method is presented.
    Keywords: AERODYNAMICS
    Type: NASA-CR-3079 , D6-43808
    Format: application/pdf
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