Research on the fixed elasticity flying of high speed aircraft
- 10.2991/icmmita-15.2015.112How to use a DOI?
- aircraft; stability; control; fixed elasticity flying; numerical simulation
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.
- © 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 - 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 -