Numerical solution of three‐dimensional viscous shock layer using axisymmetric analog along the streamlines-Reference-Cited by-同舟云学术

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Numerical solution of three‐dimensional viscous shock layer using axisymmetric analog along the streamlines

Published:2008-01-11 Issue:1 Volume:18 Page:36-49
ISSN:0961-5539
Container-title:International Journal of Numerical Methods for Heat & Fluid Flow
language:en
Short-container-title:Int Jnl of Num Meth for HFF

Author:

Noori S.,Karimian S.M.H.,Malekzadeh Dirin M.

Publisher

Emerald

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials

Reference12 articles.

1. Comparison of Hypersonic Experiments and PNS Predictions Part I: Aerothermodynamics

2. Approximate viscous shock layer technique for calculating hypersonic flows around blunt-nosed bodies

3. Approximate viscous shock-layer method for hypersonic flow over blunt-nosed bodies

4. Higher-order viscous shock-layer solutions for high-altitude flows

5. Hypersonic viscous shock-layer solutions over long slender bodies. I- High Reynolds number flows

Cited by 1 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. Viscous Shock Layer Around Slender Bodies with Nonequilibrium Air Chemistry;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2016-11-22

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