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- Kessel, T. van (author), Vanlede, J. (author), Kuijper, C. (author), Kok, J. de (author) report 2007
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- Wesenbeeck, B.K. van (author) report 2007
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- Kessel, T. van (author), Vanlede, J. (author), Kok, J. de (author) report 2007
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- Kleissen, F.M. (author), Arentz, L. (author), Reed, M. (author), Johansen, O. (author) report 2007
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- Kessel, T. van. (author), Vanlede, J. (author), Bruens, A. (author) report 2006
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- Vuren, S. van. (author), Ottevanger, W. (author) report 2006
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- Kessel, T. van. (author), Vanlede, J. (author) report 2006
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- Rijn, L.C. van (author), Walstra, D.J.R. (author), Ormondt, M. van. (author) report 2004
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- Walstra, D.J.R. (author) report 2004
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- Walstra, D.J.R. (author), Helvert, M.A.G. van (author) report 2003
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- Flokstra, C (author), Schijndel, S.A.H. van (author) report 2002
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- Goede, E.D. de (author) report 2001
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- Antoniewicz, M.R. (author), Van Maris, A.J.A. (author), Spitters, C.G.M. (author), Wu, L. (author) report 1998
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Leendertse, J.J. (author)This report describes a method for radiating disturbances generated in the computational field through the radiating boundaries. First a simulation is made without disturbances (such as a storm surge) subsequently a second simulation is made with the radiating boundary conditions activated, and the disturbance is able to pass through the...report 1997
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- Fawaz, S. (author) report 1996
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Arendsen, P. (author), van Dalen, F. (author), Bill, C. (author), Rothwell, A. (author)In a joint research project between the National Aerospace Laboratory (NLR) and the Faculty of Aerospace Engineering of Delft University of Technology (TUD) a multi-level system for the preliminary design of aircraft structures has been developed. The present system is essentially an extension of the existing Aircraft Design and Analysis System ...report 1995
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van der Burg, J.W. (author), Maseland, J.E.J. (author), Hagmeijer, R. (author), de Cock, K.M.J. (author)In this paper the capabilities of an automated CFD system which is currently available at NLR are demonstrated. Transonic flow around the AS28G wing/body configuration and hypersonic flow through a generic three-dimensional mixed-compression airbreathing inlet are simulated. An assessment of the level of automation of the current CFD-system is...report 1995
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Westland, J. (author), Hounjet, M.H.L. (author)In comparison with Euler methods unsteady inviscid transonic full potential methods are known to suffer from limitations with respect to the modeling of shock waves. In this paper unsteady 2D and 3D full potential methods are extended with the Clebsch variable model. This model represents exactly the shockgenerated entropy and vorticity. The...report 1993
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- Montauban, C.C. (author), Ven, M.F.C. (author) report 1993
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Hoeijmakers, H.W.M. (author)The physical aspects, the mathematical modeling, the development and application of computational methods for the simulation of vertical flows are described. The high-Reynolds number vortex flows considered are assumed to be steady, sub-critical and such that the structure of the flow is well-ordered and consists of thin shear layers and slender...report 1989