依据化学动力学中热力学参数与平衡常数关系得到烧蚀产物平衡常数与温度的简单关系式；
Then, the equations of balanceable constant and temperature are obtained according to the thermodynamics parameter in the chemical dynamics theory.
数值计算证实，发汗控制参数能有效地控制热层烧蚀，同时也能有效地控制热层温度。
The numerical results show that the transpiration control parameter can control the ablation and temperature of the thermal protection layer effectively.
测得驻点烧蚀边界层的温度分布与相应的理论计算结果符合较好。
The temperature profiles measured from the boundary layers at stagnation-point are reasonable in agreement with the results of theoretical calculation.
通过数值计算，得到了冲压发动机补燃室内绝热层温度分布以及烧蚀率。
The temperature contour in the insulation and the ablation rate can be obtained by the numerical simulation.
分析认为：实验中引起探测器系统破坏的主要原因是温度升高引起的烧蚀热。
Analyses show ablation heat is the most important reason of detector system damage in this experiment.
分析认为：实验中引起探测器系统破坏的主要原因是温度升高引起的烧蚀热。
Analyses show ablation heat is the most important reason of detector system damage in this experiment.
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