Generalized Scaling Analysis of the Separation Zone Induced by Shock Wave–Turbulent Boundary Layer Interactions-Reference-Cited by-同舟云学术

Generalized Scaling Analysis of the Separation Zone Induced by Shock Wave–Turbulent Boundary Layer Interactions

Published:2023-01 Issue:1 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Shu-zi¹^ORCID,Xie Wen-zhong²^ORCID,Wang Zhen-yu³^ORCID,Hu Jun⁴,Guo Shengmin⁵^ORCID

Affiliation:

1. Ph.D. Candidate, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China. ORCID: .

2. Associate Professor, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China (corresponding author). ORCID: .

3. Postgraduate, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China. ORCID: .

4. Professor, College of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, People’s Republic of China.

5. Professor, Dept. of Mechanical Engineering, Louisiana State Univ., Baton Rouge, LA 70803. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001505

Reference74 articles.

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2. Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows;Andreopoulos J.;J. Fluid Mech.,2006

3. Flow physics and sensitivity to RANS modelling assumptions of a multiple shock wave/turbulent boundary layer interaction

4. Experimental and numerical study of forced shock-wave oscillations in a transonic channel

5. Hypersonic Incident Shock-Boundary Layer Interaction Control by Wavy Patches

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