通过试验，选择了合适的结构滤波器参数，有效地抑制了飞行控制系统与飞机弹性结构之间的耦合。
Through ground test, suitable parameters of the structural filter are selected and the coupling between the flight control system and the aircraft elasticity structure is effectively restrained.
试验结果证明，复合不耦合装药结构可以降低工作面温度和减小对周围保留冻土爆破振动的损伤。
The test results have proved that the compound non-coupling charging structure can reduce the temperature of the working face and the blasting vibration damage on the reserved frozen soil.
阐述了将结构热试验和气动加热计算相结合，实现气动热分析与热试验相耦合的试验控制方法。
Based on thermo-structural experiment, coupling of aeroheating analysis and thermal test, a new experimental control method is described.
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