Research on constant attack angle flying of hypersonic aircraft

DOI

10.2991/icmmita-15.2015.110How to use a DOI?

Keywords

hypersonic aircraft; stability; control; free flying; numerical simulation

Abstract

A kind of imaginary virtual flying with numerical simulation is used to testify the rightness of hypersonic aircraft with air dynamic coefficients. Since the attack angle is the most important factor that affect the stability of the hypersonic or supersonic aircraft, so a kind of virtual flying with constant attack angle is proposed to do the open loop numerical simulation to check the air coefficients of system model. This kind of testing method is very useful for situations that the rightness of the aircraft system model is not guaranteed, especially for complex flying systems. So this new testing method is very meaningful and useful for hypersonic engineering.

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  - Guoqiang Liang
AU  - Jianhong Shi
PY  - 2015/11
DA  - 2015/11
TI  - Research on constant attack angle flying of hypersonic aircraft
BT  - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SP  - 572
EP  - 575
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-15.2015.110
DO  - 10.2991/icmmita-15.2015.110
ID  - Liang2015/11
ER  -