High-Speed Boundary-Layer Stability on a Cone with Localized Wall Heating or Cooling-Reference-Cited by-同舟云学术

High-Speed Boundary-Layer Stability on a Cone with Localized Wall Heating or Cooling

Published:2015-09 Issue:9 Volume:53 Page:2512-2524
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fedorov Alexander¹,Soudakov Vitaly,Egorov Ivan,Sidorenko Andrey²,Gromyko Yury,Bountin Dmitry,Polivanov Pavel,Maslov Anatoly

Affiliation:

1. Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, 140180, Zhukovsky, Russia

2. Hypersonic Flow Laboratory, Institute of Theoretical and Applied Mechanics, 630090, Novosibirsk, Russia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053666

Reference12 articles.

1. NeilandV.Ya BogolepovV. V.DudinG. N.LipatovI. I., Asymptotic Theory of Supersonic Viscous Gas Flows, Elsevier, 2008, pp. 120–135, Chap. 3.5.

2. Analytical and Computational Study of Wall Temperature Jumps in Supersonic Flow

3. SoudakovV. G.EgorovI. V.FedorovA. V. “Numerical Simulation of Receptivity of a Hypersonic Boundary Layer over a Surface with Temperature Jump,” Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles, ESA SP-659, Versailles, France, 2008.

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