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Design Method of Scramjet Nozzles within Predetermined Geometrical Space and Experimental Verification
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-10-08 , DOI: 10.1061/(asce)as.1943-5525.0001372 Yile Chen 1 , Kaikai Yu 2 , Guangtao Song 3 , Jianhui Ge 4 , Jinglei Xu 5
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-10-08 , DOI: 10.1061/(asce)as.1943-5525.0001372 Yile Chen 1 , Kaikai Yu 2 , Guangtao Song 3 , Jianhui Ge 4 , Jinglei Xu 5
Affiliation
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：
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...
更新日期：2021-10-08
中文翻译：
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...
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