Continuum and Kinetic Simulation of Laminar Separated Flow at Hypersonic Speeds-Reference-Cited by-同舟云学术

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Continuum and Kinetic Simulation of Laminar Separated Flow at Hypersonic Speeds

Published:2000-07 Issue:4 Volume:37 Page:499-506
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Markelov G. N.¹,Kudryavtsev A. N.¹,Ivanov M. S.¹

Affiliation:

1. Russian Academy of Sciences, 630090, Novosibirsk, Russia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3591

Reference18 articles.

1. Rarefied Gas Dynamics

Cited by 30 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. Probe influence on total pressure measurements in the zone of supersonic laminar separated flow reattachment;Thermophysics and Aeromechanics;2021-11

2. Direct simulation Monte Carlo computations and experiments on leading-edge separation in rarefied hypersonic flow;Journal of Fluid Mechanics;2019-10-02

3. Flow effects in the reattachment region of supersonic laminar separated flow;International Journal of Heat and Mass Transfer;2019-02

4. Numerical study of viscous effects on centreline shock reflection in axisymmetric flow;Physics of Fluids;2019-02

5. A direct simulation Monte Carlo study of hypersonic leading-edge separation with rarefaction effects;Physics of Fluids;2018-06

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