Ground to flight transposition of the transonic characteristics of a proposed crew rescue/crew transfer vehicle-Reference-Cited by-同舟云学术

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Ground to flight transposition of the transonic characteristics of a proposed crew rescue/crew transfer vehicle

Published:1997-06-23 Issue: Volume: Page:
ISSN:
Container-title:15th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Chalot F.¹,Hasholder J.¹,Mallet M.¹,Naim A.¹,Perrier P.¹,Ravachol M.¹,Rostand P.¹,Stoufflet B.¹,Oskam B.²,Hagmeijer R.²,e al,Chalot F.¹,Hasholder J.¹,Mallet M.¹,Naim A.¹,Perrier P.¹,Ravachol M.¹,Rostand P.¹,Stoufflet B.¹,Oskam B.²,Hagmeijer R.²,e al

Affiliation:

1. Dassault Aviation, St.-Cloud, France

2. NLR, Amsterdam, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2305

Reference14 articles.

1. and G. Roge, "Development of a finite element Navier Stokes solver with applications to turbulent and hvpersonic flows", AIAA 92-0670.

2. Winds of Change

3. number of SX4 processors Figure 2.3.2-1: overall runtimespeed-up versus

4. number of 5X4 processors Figure 2.3.2-2 :parallel efficiency versusnumber

5. 15 AIAA 97-2305

Cited by 2 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. Industrial Aerodynamics;Encyclopedia of Computational Mechanics Second Edition;2017-12-15

2. CRV-CTV aerodynamic shape definition;8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;1998-04-27

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