Direct-Numerical Simulation with the Stability Theory for Turbulent Transition in Hypersonic Boundary Layer-Reference-Cited by-同舟云学术

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Direct-Numerical Simulation with the Stability Theory for Turbulent Transition in Hypersonic Boundary Layer

Published:2023-06-18 Issue:4 Volume:24 Page:1004-1014
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Bae Hajun,Lim Jiseop,Kim Minwoo,Jee Solkeun^ORCID

Funder

Ministry of Science and ICT, South Korea

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-023-00626-z.pdf

Reference27 articles.

1. Mack LM (1984) Boundary-layer linear stability theory. Tech. rep., California Inst of Tech Pasadena Jet Propulsion Lab

2. Malik MR (1989) Prediction and control of transition in supersonic and hypersonic boundary layers. AIAA J 27(11):1487–1493

3. Fedorov A (2011) Transition and stability of high-speed boundary layers. Annu Rev Fluid Mech 43:79–95

4. Horvath T, Berry S, Merski N, Berger K, Buck G, Leichty D, Schneider S (2006) In: 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. https://doi.org/10.2514/6.2006-2919

5. Horvath T, Tomek D, Splinter S, Zalameda J, Krasa P, Schwartz R, Gibson D, Tietjen A, Berger K (2010) In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. https://doi.org/10.2514/6.2010-241

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