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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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- van-Herk, A. (author), Wesseling, P. (author) conference paper 1974
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Schellekens, L.W.M.P. (author)Some experiences with a computer program based on a version of the Woodward panel method for the calculation of aerodynamic characteristics of bodies, wings and wing-body combinations in stationary supersonic flow are described. The method is based on the linearized theory for stationary supersonic potential flow, in which the flow around the...report 1973
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Dalrymple, R.A. (author)Water wave modeIs, incorporating shear currents, are developed for linear and nonlinear waves. The first model assumes a constant vorticity over the depth of the fluid; the case for a wave propagating on a linear shear current. For greater generality, a second model is presented which assumes that the fluid is composed of two layers, each with a...report 1973
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Collignon, T.P. (author), Van Gijzen, M.B. (author)IDR(s) is a family of fast algorithms for iteratively solving large nonsymmetric linear systems [14]. With cluster computing and in particular with Grid computing, the inner product is a bottleneck operation. In this paper, three techniques are combined in order to alleviate this bottleneck. Firstly, the efficient and stable IDR(s) algorithm...report