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.
利用有限元分析结果，根据热光效应和弹光效应理论，对气动热环境下红外光学头罩的折射率场进行数值计算。
Based on the theories of thermo-optical effect and elastic-optical effect, the refractive index field of the dome was numerically computed with the result of the finite element analysis.
对热气动式微泵进行了热分析，得到了泵室压力与温度场的关系。
Thermal analysis on the thermopneumatic pump to be used in the PCR chip is performed to understand the relation between chamber pressure and temperature field.
对超高音速火箭的飞行载荷和气动热进行了分析计算。
The flight loads and dynamic heating of the rocket during flight in a high supersonic velocity are also analyzed and calculated.
对超高音速火箭的飞行载荷和气动热进行了分析计算。
The flight loads and dynamic heating of the rocket during flight in a high supersonic velocity are also analyzed and calculated.
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