Local-Variable-Based Model for Hypersonic Boundary Layer Transition-Reference-Cited by-同舟云学术

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Local-Variable-Based Model for Hypersonic Boundary Layer Transition

Published:2019-06 Issue:6 Volume:57 Page:2372-2383
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Guo Peixu¹,Gao Zhenxun¹,Zhang Zhichao¹,Jiang Chongwen¹,Lee Chun-Hian¹

Affiliation:

1. Beihang University, 100191 Beijing, People’s Republic of China

Funder

Excellence Foundation of BUAA for PhD Students

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056828

Reference42 articles.

1. RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory

2. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition

3. MackL. M. “Boundary-Layer Linear Stability Theory,” AGARD Rept. 709, 1984.

4. Reassessment of the scale-determining equation for advanced turbulence models

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