Effects of Thermo-chemical Models on Linear Stability Analysis of Chemically Reacting Hypersonic Boundary Layers-Reference-Cited by-同舟云学术

Effects of Thermo-chemical Models on Linear Stability Analysis of Chemically Reacting Hypersonic Boundary Layers

Published:2023-06-19 Issue:4 Volume:24 Page:985-1003
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Park Jaeyoung,Park Donghun^ORCID

Funder

National Research Foundation of Korea

Korea Research institute for defense Technology planning and adancement

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/s42405-023-00614-3.pdf

Reference40 articles.

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2. Brown J (2002) Turbulence model validation for hypersonic flows. In: 8th AIAA/ASME joint thermo-physics and heat transfer conference, p 3308. https://doi.org/10.2514/6.2002-3308

3. Van Driest ER (1952) Investigation of laminar boundary layer in compressive fluids using the Crocco method. NACA Technical Note 2597. https://ntrs.nasa.gov/citations/19930083425. Accessed Mar 2022

4. Malik MR (1989) Prediction and control of transition in supersonic and hypersonic boundary layers. AIAA J 27(11):1487–1493. https://doi.org/10.2514/3.10292

5. Malik MR (1998) Boundary-layer transition prediction toolkit. In: Computational fluid dynamics review 1998: (in 2 volumes), pp 869–890. https://doi.org/10.1142/9789812812957_0047

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