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- Zwaaneveld, J. (author) report 1976
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Lindhout, J.P.F. (author), de Boer, E. (author)A method is presented to compute the 3D compressible turbulent boundary layer on an adiabatic wall under infinite swept wing conditions. The mathematical model of turbulence is based on a generalisation of Bradshaw's 2D shear stress equation. This results in a system of 5 equations valid along 5 distinct characteristics. A brief discussion is...report 1975
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- Snel, H. (author), Lindhout, J. (author), Merck, W. (author), Houben, J. (author) report 1975
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Labrujère, T.E. (author), van der Vooren, J. (author)An iterative finite element calculation is presented of the subcritical CGmpressible flow about a thin parabolic arc of revolution and inside an axisymmetric air intake. The calculations were performed in tenns of the stream function as well as in terms of the velocity potential Both results for the parabolic arc of revolution are compared with...report 1974
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Smith, J. (author)The report describes experiences with the Garabedian and Korn program for the computation of compressible potential flows, with or without shocks, both supercritical shockless flows and flows with shock waves. Computations for a number of quasi-elliptical aerofoils indicated that the conformal mapping procedure should be handled with care....report 1974
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- Zwaaneveld, J. (author), van Egmond, J.A. (author) report 1972