最后在对飞机典型结构风挡、雷达罩、机尾翼前缘的试验与仿真研究的基础上，对飞机典型结构的抗鸟撞设计准则进行了探讨。
Based on test and simulation of aircraft windshield , the anti-bird impact design guide line of aircraft typical structures for radome and leading edge of wing and empennage is discussed .
雷达罩