Zhu Chengxiang
Education Level:博士研究生毕业
Alma Mater:University of Stuttgart
Paper Publications
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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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乘波前体三维内转进气道气动融合设计.推进技术,第39卷(第10期):2320-2328.
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Zhu Chengxiang,重油活塞发动机的燃烧关键技术分析.小型内燃机与车辆技术,第47卷(第2期):91-96.
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曲锥前体/三维内转进气道一体化设计与分析.航空动力学报,第33卷(第1期):87-96.
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Zhu Chengxiang,YYC,Inverse method of characteristics with given exit parameters for the computation of supersonic flows.21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,
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QRF,ZJF,Zhu Chengxiang.Compressible lattice Boltzmann simulations on high-performance and low-cost GeForce GPU.Concurrency Computation,31(20):-.
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Zhu Chengxiang,剪切稀化非牛顿射流撞击液膜破碎直接数值模拟.航空学报,第39卷(第5期):91-99.
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Zhu Chengxiang,高超声速进气道的裂解碳氢燃料提前喷注研究.推进技术,第39卷(第1期):196-202.
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QRF,Zhu Chengxiang.Lattice boltzmann simulation for supersonic/hypersonic compressible flows.21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,