Research on the fixed elasticity flying of high speed aircraft

DOI

10.2991/icmmita-15.2015.112How to use a DOI?

Keywords

aircraft; stability; control; fixed elasticity flying; numerical simulation

Abstract

The elasticity is a very special factor considered in modeling of supersonic aircraft, and it is usually neglected in supersonic aircraft. Since it will cause the force and moment of the aircraft totally different, so it increased the complexity and difficulty of hypersonic aircraft. To simplify the analysis and to testify the rightness of the air coefficients of aircraft model, a kind of fixed elasticity virtual flying condition is proposed and the numerical simulation is done with computer program according to the proposed model and coefficients. Finally, the simulation result is shown to analyze the dynamic performance and characteristic of the proposed method.

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  - Lingling Wang
AU  - Huali Wu
PY  - 2015/11
DA  - 2015/11
TI  - Research on the fixed elasticity flying of high speed aircraft
BT  - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SP  - 581
EP  - 585
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-15.2015.112
DO  - 10.2991/icmmita-15.2015.112
ID  - Wu2015/11
ER  -