Zhu Chengxiang
Education Level:博士研究生毕业
Alma Mater:University of Stuttgart
Paper Publications
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考虑来流边界层的超燃燃烧室喷射特性.航空动力学报,2016,31(06):1351-1358.
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HY,Zhu Chengxiang.Effects of incoming boundary layer on injection characteristics of a scramjet combustor.Hangkong Dongli Xuebao/Journal of Aerospace Power,2016,31(6):1351-1358.
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YYC,Zhu Chengxiang.An inverse method for supersonic flowfield with given downstream boundary.Tuijin Jishu/Journal of Propulsion Technology,2016,37(4):624-631.
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给定下游边界的超声速流场逆向求解方法.推进技术,2016,v.37;No.226(04):27-34.
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给定下游边界的超声速流场逆向求解方法.推进技术,2016,v.37;No.226(04):27-34.
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Zhu Chengxiang,横向气流中非牛顿液体射流直接数值模拟.航空学报,2016,v.37(09):42-51.
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Zhu Chengxiang,横向气流中非牛顿液体射流直接数值模拟.航空学报,2016,v.37(09):42-51.