Research on fixed attack angle attack angle and height flying of hypersonic aircraft
- 10.2991/icmmita-15.2015.111How to use a DOI?
- hypersonic aircraft;fixed attack angle; fixed height; numerical simulation
Attack angle is a most important factor that affect the stability of aircraft no matter for supersonic type or hypersonic type aircraft. And height is another factor that will affect the force and moment of the whole dynamic system by change the density of air and finally it will also affect the stability of the whole system. So in this paper a kind of virtual flying with fixed attack angle and height is proposed to testify the rightness of the hypersonic aircraft model and air coefficient. It is a new and meaningful model testifying method for complex flying systems.
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Guangbin Wu AU - Heng Li AU - Junwei Lei PY - 2015/11 DA - 2015/11 TI - Research on fixed attack angle attack angle and height flying of hypersonic aircraft BT - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 576 EP - 580 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-15.2015.111 DO - 10.2991/icmmita-15.2015.111 ID - Wu2015/11 ER -