By J. Y. Tu, C. A. J. Fletcher (auth.), Dr. Dieter Leutloff, Dr. Ramesh C. Srivastava (eds.)
Computational tools and modelling is of turning out to be value in primary technology in addition to in purposes in and in environmental examine. during this topical quantity, compiled in honor of Professor K.G. Roesner of the Darmstadt Institute of know-how, the readers locate very important contributions within the box of turbulent boundary layers, the Tsunami challenge, staff invariant resolution of hydrodynamic equations, non-linear waves, modelling of the matter of evaporation-condensation, the precise answer of discrete versions of the Boltzmann equation and so forth. The publication addresses researchers and engineers either within the mechanical sciences and in clinical computing.
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Extra info for Computational Fluid Dynamics: Selected Topics
1). 977] in laboratory experiments using a wide tank. 86"1 at the end of the first phase of the motion (Fig. 3) when the whole tank has been filled with layers. Then, the height of the layers increases as merging occurs until the three-cell configuration is attained. 015) the time-derivatives were continuously decreasing and relatively small. For example, the derivative ofthe maximum value of the vorticity satisamax(w) 3 . fies ( at /max(w) ~ 10- . Therefore, we may thmk that the three-cell configuration corresponds to a steady state.
1'il ~i ' .. - ,'I lS - - -J ! ~; \;I' 1'- _ ~ ! S):~ ~ . :. 556 lines ~. '*~ ~~ fn~ ,\,, ~ ~ !! :::::? 188 0. 300 Fig. 2. Streamlines and iso-concentration lines: first phase of the formation of layers work against gravitation. This explains why the first convective cell appears at the bottom of the tank near the heated walL Such a behaviour has been experimentally observed for exemple in , . The physical process above described was first observed in  and applied to the present problem in .
P8 - stat. isolines for e and ljf 28 Fig. 14. Kl - stat. isolines for 8 and l/I Fig. 15. K2 - stat. isolines for 8 and l/I Fig. 16. K4 - stat. isolines for 8 and l/I Fig. 17. K5 - stat. isolines for 8 and l/I Fig. 18. K4 - time history of II ~~ II Fig. 19. K5 - time history of II ~~ II 29 Fig. 20. PI/3d - 'P =0 Fig. 21. PI/3d - 'P = 11"/2 Fig. 22. PI/3d - 'P = 11" Fig. 23. PI/3d - 'P = 311"/2 =---11 » ...... lI/1J"' .. · " " · · ) / / 1111 11 " 111'' ' "",,. l\\\\\\'''·--· .. , .. ,· . . . , ..
Computational Fluid Dynamics: Selected Topics by J. Y. Tu, C. A. J. Fletcher (auth.), Dr. Dieter Leutloff, Dr. Ramesh C. Srivastava (eds.)