Computation of an underexpanded 3-D rectangular jet by the CE/SE method-Reference-Cited by-同舟云学术

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Computation of an underexpanded 3-D rectangular jet by the CE/SE method

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Loh Ching¹,Himansu Ananda¹,Wang Xiao¹,Jorgenson Philip¹

Affiliation:

1. NASA, Glenn Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-986

Reference22 articles.

1. Karypis,G.andKumar,V."Multilevelk-wayPartitioning Scheme for Irregular Graphs", Univ. of Minnesota Dept. of Comp. Sc. / Army HPC ResearchCenterTech. Report 95-064

2. The Method of Space-Time Conservation Element and Solution Element—A New Approach for Solving the Navier-Stokes and Euler Equations

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1. The improved space-time conservation element and solution element scheme for two-dimensional dam-break flow simulation;International Journal for Numerical Methods in Fluids;2011-03-02

2. Shock wave configurations and flow structures in non-axisymmetric underexpanded sonic jets;Shock Waves;2010-05-21

3. An improved CE/SE scheme for multi-material elastic–plastic flows and its applications;Computers & Fluids;2009-03

4. Rectangular underexpanded gas jets: Effect of pressure ratio, aspect ratio and Mach number;Shock Waves;2009

5. Computation of Low Speed Cavity Noise;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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