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.
应用推荐