Estimation of the Effect of Lift-drag Ratio caused by Relaxing Longitudinal Static Stability of a certain-type of Joined-Wing Aircraft
- Zhen Liang, Weijun Wang
- Corresponding Author
- Zhen Liang
Available Online March 2018.
- https://doi.org/10.2991/mecae-18.2018.118How to use a DOI?
- Joined-wing aircraft, Relaxing static stability, Lift-drag ratio.
- According to a given joined-wing aircraft, based on the DATCOM calculation data, under typical cruise and stable hover flight conditions, cases are considered with and without the relaxation of static stability technique. The actual lift-drag ratio of the joined-wing layout and conventional layout is compared and the difference is revealed. This proceeding analyses the reason, seeking the pattern, providing the foundation for the optimization of the overall program of the aircraft in the future.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Zhen Liang AU - Weijun Wang PY - 2018/03 DA - 2018/03 TI - Estimation of the Effect of Lift-drag Ratio caused by Relaxing Longitudinal Static Stability of a certain-type of Joined-Wing Aircraft BT - 2018 International Conference on Mechanical, Electronic, Control and Automation Engineering (MECAE 2018) PB - Atlantis Press UR - https://doi.org/10.2991/mecae-18.2018.118 DO - https://doi.org/10.2991/mecae-18.2018.118 ID - Liang2018/03 ER -