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Titlebook: Recent Contributions to Fluid Mechanics; Werner Haase Book 1982 Springer-Verlag Berlin Heidelberg 1982 dynamics.fluid dynamics.fluid mecha

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21#
發(fā)表于 2025-3-25 05:45:17 | 只看該作者
22#
發(fā)表于 2025-3-25 09:41:25 | 只看該作者
Some Aspects to the Structure of Separated Flowscture of dead water behind bodies with different contours is illustrated on the basis of pressure and LDA-measurements. Typical data obtained on pressure distributions, vortex structures and extensions of dead waters can serve as a basis for the development of a dead water model.
23#
發(fā)表于 2025-3-25 12:57:46 | 只看該作者
24#
發(fā)表于 2025-3-25 17:42:23 | 只看該作者
Investigation of the Three-Dimensional Transonic Flow around an Air Intake by a Finite-Volume Method°). The ratio of static pressures at channel exit and infinity has been held constant. The analysis was carried out for an isolated air intake, i.e. the fuselage is omitted and the splitter plate is extended to an infinite flat plate. The Euler equations written in integral-conservation form are sol
25#
發(fā)表于 2025-3-25 23:06:33 | 只看該作者
Calculation of a Laminar-Turbulent Two-Dimensional Turbine Blade Boundary Layer Including Surface Cuace curvature effects. The surface curvature is generally large on turbine blades. This gives rise to study this second order effect. Comparisons of first and second order calculations with a finite difference method [2] resulted in small changes of the location of the laminar or turbulent separatio
26#
發(fā)表于 2025-3-26 01:00:57 | 只看該作者
Considerations of the Vorticity Fields on Wings at the trailing edge. The resulting vortex sheet behind the wing in reality carries vorticity which is created at the wing surface due to the non-slip condition. It is discussed qualitatively how the vorticity properties of wing boundary layers fit into the picture of the potential flow model of li
27#
發(fā)表于 2025-3-26 06:25:49 | 只看該作者
28#
發(fā)表于 2025-3-26 12:24:48 | 只看該作者
29#
發(fā)表于 2025-3-26 15:01:24 | 只看該作者
30#
發(fā)表于 2025-3-26 18:53:16 | 只看該作者
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