根据高空高速飞行特点及瞬态热载荷值，确定仪器设备舱调温系统方案。
According to flight feature and transitional thermal load value, scheme of temperature adjusting system of electronic equipment cabin was presented.
阐明了热瞬态密封问题求解的关键是给出螺栓载荷的热态增量；
It expounds that the key of solving thermal transient sealing problem is to obtain the thermal increment of stud-bolt loading.
其次，在喷管轴对称模型瞬态热分析的基础上研究了轴对称载荷下热—结构耦合场的应力分析。
Next, on the basis of the transient-state thermal analysis, the thermal elastic-plastic analysis of the thermal-structure couple is obtained in the axial symmetry loads.
其次，在喷管轴对称模型瞬态热分析的基础上研究了轴对称载荷下热—结构耦合场的应力分析。
Next, on the basis of the transient-state thermal analysis, the thermal elastic-plastic analysis of the thermal-structure couple is obtained in the axial symmetry loads.
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