Analytical Solutions of Shock Structure Thickness and Asymmetry in Navier–Stokes/Fourier Framework-Reference-Cited by-同舟云学术

Analytical Solutions of Shock Structure Thickness and Asymmetry in Navier–Stokes/Fourier Framework

Published:2014-05 Issue:5 Volume:52 Page:1075-1081
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Myong R. S.¹

Affiliation:

1. Department of Aerospace and System Engineering and Research Center for Aircraft Parts Technology, Gyeongsang National University, Gyeongnam 660-701, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052583

Reference24 articles.

1. Sto�welle und Detonation

2. On a Complete Solution of the One-Dimensional Flow Equations of a Viscous, Heat-Conducting, Compressible Gas

3. The Solution of the Boltzmann Equation for a Shock Wave

4. The profile of a steady plane shock wave

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