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51#
發(fā)表于 2025-3-30 12:12:09 | 只看該作者
52#
發(fā)表于 2025-3-30 13:12:04 | 只看該作者
53#
發(fā)表于 2025-3-30 16:35:27 | 只看該作者
Cross-stresses in air, demonstrated by means of a centripetal vacuum pumpich arise from the lack of slipperiness of the parts of the liquid” as assumed by . in his Principia and taken over in the Navier-Stokes equations of classical hydrodynamics, but that there will be present, in general, also “cross-stresses,” i.e. normal stresses in the direction of the velocity of f
54#
發(fā)表于 2025-3-31 00:06:22 | 只看該作者
Analyse théorique du champ aérodynamique dans le voisinage immédiat d’un plan illimité, basée sur lanction est la solution de l’équation intégro-différentielle aux différences de L. ., restée insoluble jusqu’à présent. Nous allons montrer comment peut-on trouver la valeur approchée de la fonction de distribution, sans avoir à résoudre formellement l’équation de ., dans le cas du mouvement stationn
55#
發(fā)表于 2025-3-31 04:09:38 | 只看該作者
The turbulent boundary layer the layer the dominant large-scale motion appears to be jets of turbulent fluid which may arise from the release of the anisotropie Reynolds stresses set up by the shearing motion at the free boundary. The connection between these results and the hypothesis of wall similarity (“l(fā)aw of the wall”) is
56#
發(fā)表于 2025-3-31 06:53:19 | 只看該作者
Synthetic method for boundary layer thicknessin viscous flow both tangential and normal velocities must be zero. Linearization of the Navier-Stokes equations, either by regarding the fluid non-viscous or the motion to be so slow that the inertia terms can be completely or partially ignored, has resulted in only limited applications of the theo
57#
發(fā)表于 2025-3-31 10:52:44 | 只看該作者
On rotating laminar boundary layersayers at the equator were infinitely thick with zero longitudinal components of velocity but his view was that this would be unlikely in the exact solution. In any case the boundary layers from the two poles must meet at the equator and the parabolic nature of their governing equations made them ina
58#
發(fā)表于 2025-3-31 14:12:31 | 只看該作者
On laminar wall jetsr heated, if it is assumed that the coefficient of viscosity is proportional to the temperature, and his results are briefly discussed, with his permission. Finally, consideration is given to perturbations of the basic similarity solution due to a small external flow, as might arise as a consequence
59#
發(fā)表于 2025-3-31 20:04:26 | 只看該作者
Zur Bestimmung der Temperaturverteilung in dünnen Platten mit anliegender überschallgrenzschichtrmeübergang) nur sehr wenig von dem Druckfall l?ngs des K?rpers ab, aber auch nur wenig von der Str?mungsform: laminar oder turbulent. Deshalb treten im station?ren Zustand nur dann gr??ere Unterschiede in der Wandtemperatur auf, wenn die W?rmestrahlung bedeutend wird. Anders bei instation?ren Zust?
60#
發(fā)表于 2025-3-31 23:48:24 | 只看該作者
Cross-stresses in air, demonstrated by means of a centripetal vacuum pumptico-viscous cross-stresses. . and . (1956, 1957) have used this phenomenon for the design of a centripetal air pressure pump, but . (1957) has shown that such cross-forces can result from (A) a slight error in the perpendicularity of the plane of either the stator or the rotor to the axis of rotati
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