Interaction between Shock Wave and Boundary Layer in Nonequilibrium Hypersonic Rarefied Flow
Author:
Affiliation:
1. Space Transportation Engineering Department, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
2. Department of Mechanical Engineering, The University of Tokyo
Publisher
Japan Society of Mechanical Engineers
Subject
Fluid Flow and Transfer Processes,Physical and Theoretical Chemistry,Mechanical Engineering
Link
http://www.jstage.jst.go.jp/article/jsmeb/49/3/49_3_771/_pdf
Reference21 articles.
1. Interaction between a Shock Wave and a Boundary Layer in a Nonequilibrium Hypersonic Rarefied Flow. 2nd Report. Comparison of State for Translational and Rotational Energy Distributions.
2. Interaction between a Shock Wave and a Boundary Layer in a Nonequilibrium Hypersonic Rarefied Flow. 3rd Report. Effects of Gas-Surface Interaction Model.
3. Dynamic molecular collision (DMC) model for rarefied gas flow simulations by the DSMC method
4. Multistage gas–surface interaction model for the direct simulation Monte Carlo method
Cited by 2 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. Monte Carlo Simulation of Hypersonic Rarefied Gas Flow using Rotationally and Vibrationally Inelastic Cross Section Models;AIP Conference Proceedings;2011
2. The use of molecular spectra simulation for diagnostics of reactive flows;Journal of Aerospace Technology and Management;2011
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