Streamwise Vortices from Controlled Roughnesses on a Cone-Cylinder-Flare at Mach 6-Reference-Cited by-同舟云学术

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Streamwise Vortices from Controlled Roughnesses on a Cone-Cylinder-Flare at Mach 6

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Wagner Lauren N.¹,Schneider Steven P.¹,Jewell Joseph S.¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1671

Reference18 articles.

1. Shock Wave–Boundary-Layer Interactions

2. Effects of Roughness on Hypersonic Boundary-Layer Transition

3. Görtler Vortices

4. Ginoux, J. “Investigation of Flow Separation over Ramps at M=3,” Tech. Rep. AEDC-TR-65-273, Von Karman Gas Dynamics Facility, Arnold Engineering Development Center, 1965.

Cited by 4 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. Nonlinear Evolution of Instabilities in a Laminar Separation Bubble at Hypersonic Speeds;AIAA Journal;2024-05

2. Nosetip bluntness effects on a cone-cylinder-flare at mach 6;Experiments in Fluids;2024-04-30

3. Scaling and Transition Effects on Hollow-Cylinder/Flare SBLIs in Wind Tunnel Environments;AIAA SCITECH 2024 Forum;2024-01-04

4. Influence of Single Roughness Element on Hypersonic Boundary-Layer Transition of Cone;AIAA Journal;2023-07

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