Compilation and Analysis of Second Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels-Reference-Cited by-同舟云学术

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Compilation and Analysis of Second Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
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Author:

Marineau Eric C.¹,Grossir Guillaume²,Wagner Alexander³,Leinemann Madlen⁴,Radespiel Rolf⁴,Tanno Hideyuki⁵,Wadhams Tim P.⁶,Chynoweth Brandon C.⁷,Schneider Steven P.⁷,Wagnild Ross⁸,Casper Katya M.⁸

Affiliation:

1. Arnold Engineering Development Complex

2. von Kármán Institute for Fluid Dynamics

3. German Aerospace Center (DLR)

4. Technical University of Braunschweig

5. Japan Aerospace Exploration Agency (JAXA)

6. CUBRC

7. Purdue University

8. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0349

Reference38 articles.

1. Measurements and Computations of Second-Mode Instability Waves in Several Hypersonic Wind Tunnels

2. Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6

3. Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10

4. Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited)

Cited by 2 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. Influence of Nose-Tip Bluntness on Conical Boundary-Layer Instabilities at Mach 10;AIAA Journal;2019-09

2. Boundary Layer Transition on a Generic Model of Control Flaps in Hypersonic Flow;AIAA Scitech 2019 Forum;2019-01-06

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