An Approach to Shock Envelope Grid Tailoring and Its Effect on Reentry Vehicle Solutions-Reference-Cited by-同舟云学术

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An Approach to Shock Envelope Grid Tailoring and Its Effect on Reentry Vehicle Solutions

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Saunders David¹,Yoon Seokkwan²,Wright Michael²

Affiliation:

1. ELORET Corporation

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-207

Reference10 articles.

1. 2Davies,C.B. andVenkatapathy,E,"SAGE:TheSelf-AdaptiveGridCode,"NASATM1999-208792,1999.

2. 4Cheatwood, F. M. and Gnoffo, P. A. "User's Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA),"NASA TM4674,April1996.

3. Data-Parallel Line Relaxation Method for the Navier-Stokes Equations

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