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Titlebook: Recent Developments in Turbulence Management; K.-S. Choi Book 1991 Springer Science+Business Media Dordrecht 1991 management.turbulence

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41#
發(fā)表于 2025-3-28 18:20:58 | 只看該作者
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44#
發(fā)表于 2025-3-29 06:20:30 | 只看該作者
Nonlinear evolution of modes in the flow over compliant surfaces(1990) is extended to include nonlinear effects and a set of equations describing the spatial/temporal evolution of the disturbance is obtained. It is shown that there is a strong similarity between the nonlinear evolution of the Travelling Wave Flutter modes and the nonlinear evolution of the invis
45#
發(fā)表于 2025-3-29 08:18:22 | 只看該作者
On conditions of modelling and choice of viscoelastic coatings for drag reductionpothesis of the energy absorption isn’t explain a cause of facts of the friction increase. According to the interference theory,the action of viscoelastic boundary is critical. It can lead to decrease or increase of the turbulent energy generation in dependence of the wave properties of a surface. M
46#
發(fā)表于 2025-3-29 13:07:36 | 只看該作者
Experimental investigation of one-layer viscoelastic coatings action on turbulent friction and wall jointly with measurement of mechanical characteristics of these coatings under conditions, which are equivalent to the coating work in a flow. Complex carried out study, allowed to analyze the viscoelastic coating work in turbulent flow. This analysis testifies a validity of interference theory of
47#
發(fā)表于 2025-3-29 19:01:54 | 只看該作者
0926-5112 gs on drag reduction in engineering flows. The main objective of this meeting was to discuss up-to-date results of drag reduction research carried out in Europe. The organiser has adopted the philosophy of discussing the yesterday‘s results rather than the last year‘s results. No written material ha
48#
發(fā)表于 2025-3-29 20:56:53 | 只看該作者
49#
發(fā)表于 2025-3-30 02:24:53 | 只看該作者
50#
發(fā)表于 2025-3-30 07:59:00 | 只看該作者
Nonlinear evolution of modes in the flow over compliant surfaces shown that there is a strong similarity between the nonlinear evolution of the Travelling Wave Flutter modes and the nonlinear evolution of the inviscid modes in the stability of hypersonic boundary layers. The evolution equations are solved numerically and several results are presented.
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