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对非定常超音速飞行条件下尾翼片气动加热温度分布给出了一般的数值计算方法．对某翼型尾翼片在典型弹道飞行时进行了具体计算，所得结果合理．
The numerical calculation method of aerodynamic heating temperature of tail fin under unsteady supersonic flight conditions is given. The calculation results of a certain airfoil tail fin during a typical ballistic flight are reasonable.