字里行间 发表于 2025-3-21 19:01:03

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Offbeat 发表于 2025-3-21 21:18:32

The Local Vorticity Content of a Shear Layer,ign work. At that time very much discussed was the fact that at delta wings with sharp leading edges lee-side vortices resulted in the relevant angle of attack and Mach number regime. The question was, where is the apparent vorticity coming from, and accordingly the associated entropy rise.

愤怒事实 发表于 2025-3-22 02:29:55

About the Kutta Condition, surfaces. That can be the “zero thickness” trailing edge of a largeaspect-ratio wing or the “sharp” leading edge of a delta wing. Usually it is assumed that the flow leaves the trailing edge in bisector direction.

向外才掩饰 发表于 2025-3-22 07:49:03

Topology of Skin-Friction and Velocity Fields,is. In practice, however, normally not much use is made of topological analysis, maybe because it is often treated in a rather formalistic way. In view of the topic of this book we intend to accentuate the practical rather than the theoretical side of the field of topology. Even this will be made on

细菌等 发表于 2025-3-22 12:45:32

Large Aspect-Ratio Wing Flow,io wings in view mostly of the results and insights gained in Chap. 4. Considered always is the clean-wing situation, selected topics of the real-wing situation (high-lift system, integrated engines etc.) are presented in Chap. 9.

小画像 发表于 2025-3-22 13:55:08

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appall 发表于 2025-3-22 17:07:22

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figurine 发表于 2025-3-23 00:27:50

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钱财 发表于 2025-3-23 04:52:30

Ernst Heinrich Hirschel,Arthur Rizzi,Christian Breitsamter,Werner Staudacher

容易做 发表于 2025-3-23 07:06:35

Ernst Heinrich Hirschel,Arthur Rizzi,Christian Breitsamter,Werner Staudacher
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查看完整版本: Titlebook: Separated and Vortical Flow in Aircraft Wing Aerodynamics; Basic Principles and Ernst Heinrich Hirschel,Arthur Rizzi,Werner Stauda Book 202