Compressible boundary-layer computation by the method of weighted residuals using exponentials.
Author:
Affiliation:
1. Deutsche Forschungs- und Versuchsanstalt fur Luft- und Raumfahrt, Porz-Wahn, Germany
2. University of California, Santa Barbara, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference16 articles.
1. GENERAL METHOD OF INTEGRAL RELATIONS AND ITS APPLICATION TO BOUNDARY LAYER THEORY
2. Nonsimilar Solutions of the Compressible-Laminar Boundary-Layer Equations With Applications to the Upstream-Transpiration Cooling Problem
3. Approximate solution of the laminar boundary- layer equations with mass transfer.
4. Analytical prediction of the incompressible turbulent boundary layer with arbitrary pressure distribution (Incompressible two dimensional turbulent boundary layer equations with arbitrary pressure distribution solved by weighted residual method)
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1. Simulationsmodelle;Simulation dynamischer Systeme;1989
2. Simulationsmodelle;Systemdynamik;1987
3. A finite difference-Galerkin finite element solution of compressible laminar boundary-layer flows;International Journal for Numerical Methods in Engineering;1978
4. A Galerkin method for a class of steady, two-dimensional, incompressible, laminar boundary-layer flows;Journal of Fluid Mechanics;1975-06-24
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