Overview of Ares-I CFD Ascent Aerodynamic Data Development And Analysis Based on USM3D-Reference-Cited by-同舟云学术

Overview of Ares-I CFD Ascent Aerodynamic Data Development And Analysis Based on USM3D

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Abdol-Hamid Khaled¹,Ghaffari Farhad¹,Parlette Edward²

Affiliation:

1. NASA Langley Research Center

2. ViGYAN, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-15

Reference29 articles.

1. NASA'sExploration SystemsArchitecture Study.NASA-TM-2005-214062,Nov.2005.

2. Alexandrov N. M.; Atkins H. L.; Bibb K. L.; Biedron R. T.; Carpenter, M. H.; Gnoffo P. A.; Hammond D. P.; Jones W. T.; Kleb W. L.; Lee-Rausch E.M.; Nielsen E.J.; Park M.A.; Raman; V. V.; Roberts T. W.; Thomas J. L.; Vatsa V. N.; Viken S. A.; White J. A.; Wood W. A. "Team Software Development for Aerothermodynamic and Aerodynamic Analysis and Design",NASATM-2003-212421,November2003.

3. P.G. Buning; W. M. Chan; K. J. Renze; D. L. Sondak; I.T. Chiu; and J. P. Slotnick; OVERFLOW User's Manual, Version 1.6ab, 26 January 1993, NASA Ames Research Center,MoffettField,CA,Jan.1993.

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