该控制器应用于变后掠机翼的结构强度加载控制系统之中。
This controller is applied to the structural strength loading control system, which is the experimental system of a variable swept aircraft wing.
从理论及实验两方面，研究了带外挂后掠机翼的极限环颤振分叉现象，得到了稳定、半稳定及不稳定极限环。
Both theoretical and experimental analyses are performed to investigate the limit cycle flutter bifurcation of a sweepback wing with an external store in the tip of the wing.
是的，他们抄袭这些，是的就像图片里这样：有后掠机翼，有飞行员的舱盖，有双尾翼和…啊哦，引擎的数量不匹配。
Yah, just look at the pics: It has swept wings, a pilot's canopy, twin tails and… oops, the number of engines don't match.
是的，他们抄袭这些，是的就像图片里这样：有后掠机翼，有飞行员的舱盖，有双尾翼和…啊哦，引擎的数量不匹配。
Yah, just look at the pics: It has swept wings, a pilot's canopy, twin tails and… oops, the number of engines don't match.
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