Searched for: author%3A%22Spekreijse%2C+S.P.%22
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document
Kok, J.C. (author), Van Muijden, J. (author), Burgers, S.S. (author), Dol, H. (author), Spekreijse, S.P. (author)
Scientific enhancement of the analysis of thermal comfort aspects in aircraft cabins is the subject of the current investigation. For this purpose, three important processes are identified that play a significant role in thermal comfort, viz. the human response to its thermal environment which is also known as thermoregulation, the actual...
conference paper 2006
document
Spekreijse, S.P. (author), Prananta, B.B. (author), Kok, J.C. (author)
A grid deformation method has been developed for the movement of multiblock, structured grids due to surface deformation arising from aeroelastics or design optimisation. The method uses a volume spline interpolation technique to compute the deformation of block vertices and block edges. After that, the deformation of block-faces is computed by...
report 2002
document
Spekreijse, S.P. (author), Venis, A.C.J. (author)
report 1991
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Venis, A.C.J. (author), Spekreijse, S.P. (author)
report 1991
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Spekreijse, S.P. (author), Venis, A.C.J. (author)
An efficient Roe-type flux-difference scheme for chemically reacting inviscid compressible flow in thermal equilibrium is presented. The numerical scheme is validated. Three well known chemical models are compared. The set of testcases concerned quasi one-dimensional hypersonic nozzle flows, with and without strong normal Shockwaves.
report 1990
document
Spekreijse, S.P. (author)
doctoral thesis 1987
Searched for: author%3A%22Spekreijse%2C+S.P.%22
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