建立带吊挂直升机飞行操纵性分析的理论分析模型。
To analyze the handling quality of a helicopter with the heavy slung-load, this paper presents a theoretical analysis model.
根据理论分析模型，实际模拟了输出光斑的光能分布与光学扩展量的关系曲线。
By the simulation of a theoretical model, the facular intensity distribution curve versus etendue is achieved.
以锚索拔出为对象建立理论分析模型，对岩锚界面端部的断裂力学行为进行了研究。
A pullout model is set up in this paper and the fracture theory is employed to analyze the singular stress fields in the proximity of the interface ends.
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