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Titlebook: New Results in Numerical and Experimental Fluid Mechanics; Contributions to the Horst K?rner,Reinhard Hilbig Book 1997 Friedr. Vieweg & Soh

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51#
發(fā)表于 2025-3-30 09:10:13 | 只看該作者
Cooperation Project Aeronautical Researchraft industry is several times that spent in Europe. The German aeronautical research programme attempts to compensate for this disadvantage by greater efficiency. For this purpose, a close network is being established within which companies, universities and the national aerospace agency cooperate
52#
發(fā)表于 2025-3-30 13:28:07 | 只看該作者
Reduction of Aerodynamic Drag (RaWid) in the national Research and Technology Programme for Aeronautan ministry for education, research and technology since July 1, 1995. Connected to this industrial programme are the cooperation programmes “MEGAFLOW” under leadership of the DLR and “Transition” by the DFG, and several contributions by DLR and universities..The programme is oriented towards techno
53#
發(fā)表于 2025-3-30 17:25:25 | 只看該作者
National CFD Project MEGAFLOWa dependable and efficient numerical tool for the aerodynamic simulation of complete aircraft in cruise as well as in start and landing configurations, which meets the requirements for industrial implementation. This requires a concentrated cooperation with the aircraft industry, DLR and universitie
54#
發(fā)表于 2025-3-30 22:00:19 | 只看該作者
55#
發(fā)表于 2025-3-31 02:44:52 | 只看該作者
The Development of Advanced Internal Balances for Cryogenic and Conventional Tunnelsbility of the balance is the key factor in this test technology. The urgent requirement for more and more accuracy of force testing leads to a demand for more and more balance accuracy. The most urgent demand in this field comes from the Cryogenic Tunnels like the new European Wind Tunnel. Funding f
56#
發(fā)表于 2025-3-31 05:13:06 | 只看該作者
57#
發(fā)表于 2025-3-31 12:38:53 | 只看該作者
58#
發(fā)表于 2025-3-31 13:27:44 | 只看該作者
Stability Analysis of two- and three-dimensional Boundary Layer Flows with varied Wall Temperaturesty of boundary-layers in air. Our work is based on numerical analysis, and is motivated by previous experimental observations that have shown a net stabilizing effect in subsonic two-dimensional boundary layers when thin heating strips are introduced near the stagnation region. Our focus is specific
59#
發(fā)表于 2025-3-31 20:18:43 | 只看該作者
60#
發(fā)表于 2025-3-31 22:45:27 | 只看該作者
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