Transition research in the Boeing/AFOSR Mach-6 quiet tunnel

Author:

Schneider S.1,Skoch C.,Rufer S.,Matsumura S.,Swanson E.

Affiliation:

1. Purdue Univ., West Lafayette, IN

Publisher

American Institute of Aeronautics and Astronautics

Cited by 8 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. Development of Aerodynamic Design of Hypersonic Quiet Nozzles;Procedia Engineering;2015

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

3. Disturbances from Shock/Boundary Layer Interactions Affecting Upstream Hypersonic Flow;35th AIAA Fluid Dynamics Conference and Exhibit;2005-06-06

4. Numerical Analysis of the Bleed Slot Design of the Purdue Mach 6 Wind Tunnel;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

5. Bypass Transition on the Nozzle Wall of the Boeing/AFOSR Mach-6 Quiet Tunnel;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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