The formula for calculating the landing work, displacement at the wing tip, the shears and bending moments of the wing of a flexible airplane are also given.
还给出了大柔性飞机着陆功量、机翼位移、剪力、弯矩计算公式。
From an overall point of view, structure deformation of airplane must be considered and optimization design must be used in landing gear design of a flexible airplane.
算例结果表明大柔性飞机的起落架设计有必要考虑机体结构弹性,并从全局出发,采用特殊的构造措施和优化设计技术。
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