A new design method of scramjet nozzles within predetermined geometrical space is proposed to optimize the nozzle aerodynamic performance. The main characteristic of the proposed method is that the design factors and flow angle are employed to ...

中文翻译：

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预定几何空间内超燃冲压喷嘴的设计方法及实验验证

提出了一种在预定几何空间内设计超燃冲压发动机喷嘴的新方法，以优化喷嘴的气动性能。该方法的主要特点是利用设计因素和流动角...