Significant Supersonic Modes and the Wall Temperature Effect in Hypersonic Boundary Layers-Reference-Cited by-同舟云学术

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Significant Supersonic Modes and the Wall Temperature Effect in Hypersonic Boundary Layers

Published:2019-04 Issue:4 Volume:57 Page:1552-1566
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Knisely Carleton P.¹,Zhong Xiaolin¹

Affiliation:

1. University of California, Los Angeles, Los Angeles, California 90095

Funder

Office of Naval Research Global

Directorate for Engineering

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057775

Reference48 articles.

1. Hypersonic Stability and Transition

2. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers

3. Transition and Stability of High-Speed Boundary Layers

4. MackL. M. “Boundary Layer Linear Stability Theory,” AGARD TR 709, Neuilly sur Seine, France, 1984.

5. MorkovinM. V. “Transition at Hypersonic Speeds,” NASA CR 178315, 1987.

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