Flow criterion was introduced for stagnation point region and the body of the vehicle.
对驻点区和飞行器表面不同的流动区域给出了流态划分准则。
The temperature profiles measured from the boundary layers at stagnation-point are reasonable in agreement with the results of theoretical calculation.
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.
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。
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