landing angle

The load of aircraft after landing was investigated by different vertical velocities,horizontal velocities and landing elevations.

分析了不同降落速度、飞行速度和降落仰角下,飞机水面降落时机身压强随时间的变化规律。

The influence of landing at large attack angle on the load distribution of a four-wheel landing gear is studied in detail,and a method for calculating the load distribution .

本文依据飞机着陆过程中起落架的缓冲器与轴向载荷的关系曲线,在建立了机轮轮胎压缩量与飞机地面垂直载荷关系曲线的基础上,探讨了飞机大迎角着陆过程中对四轮小车式起落架前、后机轮载荷分配的影响,提出了四轮小车式起落架机轮载荷分配的计算分析方法,并以波音707飞机为例进行了计算,验证了文中所提出方法的有效性和可行性。