本文用前三种方法计算受气功加热的机身实心框的温度分布，井与全尺寸试验结果比较，得出满意的结果。这说明文中采用的各种处理方法是可行的。
This paper calculates the temperature distribution in plate frame of fuselage subjected to aerodynamic heating by means of the former three methods. The numerical results turn out to compare f…
本文用前三种方法计算受气功加热的机身实心框的温度分布，井与全尺寸试验结果比较，得出满意的结果。这说明文中采用的各种处理方法是可行的。
This paper calculates the temperature distribution in plate frame of fuselage subjected to aerodynamic heating by means of the former three methods. The numerical results turn out to compare f…
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