Finally, the surface temperature distribution and infrared radiation intensity of a given space target are calculated numerically and analyzed.
最后对国外某型空间目标的表面温度场分布和红外辐射强度分布进行了数值计算并加以分析。
The experimental behavior of a high-temperature heat pipe fin was described during startup and running with the different power. The surface temperature distribution was given.
对高温热管翅在不同功率下起动与运行性能进行实验研究，给出各种功率下高温热管翅的壁面温度分布及相应的温差分布。
The results in surface temperature distribution of a reduced scale model from the above calculation com - pared with that from experimental measurement are relatively identical.
对缩小了的床身结构用差分法求出温度分布，和表面温度实验测定值比较，得到基本相符的结果。
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