|
|
|
|
|
Zhiwei Chen, Yuxue Ge, Jie Yuan and Yang Pei
In hostile environments, engine damage is of particular concern since the engine is the only component to generate thrust that affects survivability. For an aircraft suffering thrust failure, the forced landing sites should be identified within the glidi...
ver más
|
|
|
|
|
|
|
|
|
|
|
Jingxin Guan, Jun Huang, Lei Song and Xiaoqiang Lu
To find a trajectory with low radar detection probability for stealth aircraft under the assumption of 2D space, performing a rapid turning maneuver is a useful way to reduce the radar detection probability of an aircraft by changing the azimuth angle ra...
ver más
|
|
|
|
|
|
|
|
|
|
|
Yitao Wang, Teng Zhang, Yuting He, Jiyuan Ye, Hanzhe Zhang and Xianghong Fan
A two-stage light gas gun was used to conduct a high-velocity impact test on the aircraft?s typical composite/metal connecting structure (CFRP/AL). The battle damage simulations used for the CFRP/AL connecting structure were carried out under different i...
ver más
|
|
|
|
|
|
|
|
|
|
|
Mohsen Rostami, Julian Bardin, Daniel Neufeld and Joon Chung
In considering aircraft design, it is very important to effectively size the tail configuration for stability and control. Multidisciplinary design optimization (MDO) focuses on the use of numerical optimization in the design of systems with multiple sub...
ver más
|
|
|
|
|
|