Research on fixed attack angle attack angle and height flying of hypersonic aircraft

DOI

10.2991/icmmita-15.2015.111How to use a DOI?

Keywords

hypersonic aircraft;fixed attack angle; fixed height; numerical simulation

Abstract

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.

Copyright

© 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/).

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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  -