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van Beek, F.E. (author), Bergmann Tiest, WM (author), Mugge, W. (author), Kappers, A.M.L. (author)
In a previous study, we found the perception of force magnitude to be anisotropic in the horizontal plane. In the current study, we investigated this anisotropy in three dimensional space. In addition, we tested our previous hypothesis that the perceptual anisotropy was directly related to anisotropies in arm dynamics. In experiment 1, static...
journal article 2015
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van Beek, T. (author)
lecture notes 2008
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van Beek, T. (author), van Terwisga, T.J.C. (author)
conference paper 2006
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van Beek, T. (author)
journal article 2005
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Boelens, O.J. (author), Laban, M. (author), van Beek, C.M. (author), van der Leeden, R. (author)
In this report the contribution of the National Aerospace Laboratory NLR to the 'CFD Drag Prediction Workshop' organized by the AIAA in Anaheim, CA, on June 9-10, 2001, is presented. This contribution consists of both the results of all test cases and a discussion on the accurate computations of drag coefficients. Two approaches are presented...
report 2001
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van Beek, A. (author)
doctoral thesis 2000
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van Beek, T. (author), Janssen, A. (author)
conference paper 2000
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van Beek, P.J.L. (author)
doctoral thesis 1995
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van Beek, A.J.J. (author), Dijkstra, A.H. (author), Koldewe, G. (author)
In this report a model for the tectonic evolution of the Sarmatian Shield (Ukraine, Belarussia and part of Russia) is developed, in order to explain the location and orientation of the Devonian Pripyat-Dniepr-Donets palaeorift, which is transsecting the Sarmatian Shield and to derive a genetic model for the rift-hosted mercury-antimony deposits....
report 1995
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van Beek, T. (author)
conference paper 1995
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van Beek, A. (author)
doctoral thesis 1995
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de Boorder, H. (author), van Beek, A.J.J. (author), Dijkstra, A.H. (author), Galetsky, L.S. (author), Koldewe, G. (author), Panov, B.S. (author)
report 1994
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Blok, Jan J. (author), van Beek, S. (author)
report 1991
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van Beek, C.M. (author)
The application of a boundary integral or "panel" method to duct flows is described. The method is capable of computing the three dimensional, steady state, subsonic, linearized (Prandtl-Glauert) potential flow about general configurations. The method is characterized by the application of a Dirichlet boundary condition and of "compressible"...
report 1987
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van Beek, C.M. (author), Piers, W.J. (author), Slooff, J.W. (author)
A boundary integral or "panel" method is described for computing the threedimensional, steady state, potential flow about ship configurations with or without lifting surfaces in the presence of a free surface in an initially undisturbed sea. The low order method is characterized by a special modelling of the free surface boundary condition, by...
report 1985
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van Beek, G.E. (author)
report 1984
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van Beek, H.J.T. (author)
report 1980
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van Beek, T. (author)
master thesis 1980
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van Beek, A.W. (author)
report 1973
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