Numerical Simulation Study of Aerodynamic Characteristic on Hypersonic Aircraft
Jiang Chen, Song-ping Wu
Available Online November 2012.
- https://doi.org/10.2991/citcs.2012.130How to use a DOI?
- hypersonic; aerodynamic characteristic; numerical simulation
- 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.
- 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 -