Proceedings of the 2012 National Conference on Information Technology and Computer Science

Numerical Simulation Study of Aerodynamic Characteristic on Hypersonic Aircraft

Authors
Jiang Chen, Song-ping Wu
Corresponding Author
Jiang Chen
Available Online November 2012.
DOI
https://doi.org/10.2991/citcs.2012.130How to use a DOI?
Keywords
hypersonic; aerodynamic characteristic; numerical simulation
Abstract
In this paper, a three dimension model that is similar to the hypersonic cruise aircraft X-51A has been generated by using a graphics processing technology and an anti-modeling method from the published pictures and related articles about the X-51A. This paper adopts the Harten-Yee's scheme to simulate the aircraft at the cruise state of M'=6, '=6. And related results are acquired. Analyze the basic characteristics of the flow-field qualitatively and find that the result is kept well with the designed state. So it means that the model could be used for the further related research.
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Proceedings
2012 National Conference on Information Technology and Computer Science
Part of series
Advances in Intelligent Systems Research
Publication Date
November 2012
ISBN
978-94-91216-39-8
ISSN
1951-6851
DOI
https://doi.org/10.2991/citcs.2012.130How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Jiang Chen
AU  - Song-ping Wu
PY  - 2012/11
DA  - 2012/11
TI  - Numerical Simulation Study of Aerodynamic Characteristic on Hypersonic Aircraft
BT  - 2012 National Conference on Information Technology and Computer Science
PB  - Atlantis Press
SP  - 507
EP  - 509
SN  - 1951-6851
UR  - https://doi.org/10.2991/citcs.2012.130
DO  - https://doi.org/10.2991/citcs.2012.130
ID  - Chen2012/11
ER  -