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Source Publication：18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012
Creator：岳连捷
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Document Type：会议论文
Community：高温气体动力学国家重点实验室
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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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Submit date：2014/02/24
