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Shape design to minimize the peak heat-flux of blunt leading-edge 会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Cui K(崔凯)
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Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Chen LH(陈立红);  Zhang XY(张新宇);  Xiao YB(肖雅彬)
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Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
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Modeling and measurements of heat release distributions in dual-mode scramjet combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Tian L(田璐);  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian L(田璐)
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