Characterization of Post-shock Thermal Striations on a Cone/Flare-Reference-Cited by-同舟云学术

Characterization of Post-shock Thermal Striations on a Cone/Flare

Published:2020-05 Issue:5 Volume:58 Page:2352-2358
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Running Carson L.,Juliano Thomas J.,Borg Matthew P.,Kimmel Roger L.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference25 articles.

1. Hypersonic and High-Temperature Gas Dynamics, Second Edition

2. ArnalD.DéleryJ. “Laminar-Turbulent Transition and Shock Wave/Boundary Layer Interaction,” the von Karman Inst., TR-RTO-EN-AVT 116, Rhode-St-Genese, Belgium, Dec. 2005.

3. Reattachment streaks in hypersonic compression ramp flow: an input–output analysis

4. RogheliaA.ChuvakhovP.OlivierH.EgorovI. “Experimental Investigation of Görtler Vortices in Hypersonic Ramp Flows Behind Sharp and Blunt Leading Edges,” AIAA Paper 2017-3463, June 2017. 10.2514/6.2017-3463

5. Streamwise vortices in reattaching high-speed flows - A suggested approach

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