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。
