Numerical Analysis of the Bleed Slot Design of the Purdue Mach 6 Wind Tunnel

Author:

Taskinoglu Ezgi1,Knight Doyle1,Schneider Steven2

Affiliation:

1. Rutgers University

2. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Design and qualification of a supersonic wind tunnel for induced boundary layer transition research;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2014-06-10

2. Development of Hypersonic Quiet Tunnels;Journal of Spacecraft and Rockets;2008-07

3. Quiet-Flow Ludwieg Tube for Hypersonic Transition Research;AIAA Journal;2008-07

4. The Development of Hypersonic Quiet Tunnels;37th AIAA Fluid Dynamics Conference and Exhibit;2007-06-15

5. Bleed Lip Geometry Effects on the Flow in a Hypersonic Wind Tunnel;AIAA Journal;2006-09

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