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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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高温气体动力学研究进... [1]
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Source Publication：高温气体动力学研究进展
Creator：yangguowei分杨国伟
Date Issued：2011
Community：高温气体动力学国家重点实验室
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双发动机高超声速乘波飞行器性能分析
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
崔凯
;
高太元
;
胡守超
;
王秀平
;
杨国伟
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Submit date：2014/01/23
高超声速
乘波体
升阻比
计算流体力学
