Numerical Simulation of the Influence of a Mach Wave on the Laminar–Turbulent Transition in a Supersonic Boundary Layer-Reference-Cited by-同舟云学术

Numerical Simulation of the Influence of a Mach Wave on the Laminar–Turbulent Transition in a Supersonic Boundary Layer

Published:2022-05 Issue:5 Volume:67 Page:144-147
ISSN:1028-3358
Container-title:Doklady Physics
language:en
Short-container-title:Dokl. Phys.

Author:

Egorov I. V.,Ngoc Hai Duong ,Nhu Can Nguyen ,Palchekovskaya N. V.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

https://link.springer.com/content/pdf/10.1134/S1028335822050019.pdf

Reference11 articles.

1. S. A. Gaponov and A. A. Maslov, Development of Disturbances in Compressible Flows (Nauka, Novosibirsk, 1980) [in Russian].

2. J. Laufer, Aerospase Sci. 28, 685 (1961).

3. J. M. Kendall, AIAA J. 13, 290 (1975).

4. V. G. Pridanov, A. M. Kharitonov, and V. V. Chernykh, Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1, 160 (1974).

5. V. Ya. Borovoi, I. V. Egorov, V. E. Mosharov, A. S. Skuratov, and V. N. Radchenko, Extreme Heating of Bodies in a Hypersonic Flow (Nauka, Moscow, 2018) [in Russian].

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Features of the cross-correlation characteristics of disturbances in the supersonic boundary layer of the plate at the influence of a pair of weak shock waves on the leading edge;Thermophysics and Aeromechanics;2024-07-29

2. Influence of the leading-edge bluntness radius of a plate on the response of flat-plate boundary layer to an N-wave at Mach number M = 2;Thermophysics and Aeromechanics;2023-08-17

3. EXPERIMENTAL STUDY OF EVOLUTION OF CONTROLLED PERTURBATIONS IN A LONGITUDINAL VORTEX GENERATED IN A BOUNDARY LAYER ON A FLAT PLATE AT A MACH NUMBER M = 2;Journal of Applied Mechanics and Technical Physics;2023-08