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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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力学所知识产出(19... [4]
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王发民 [5]
丁海河 [2]
刘嘉 [1]
姚文秀 [1]
李立伟 [1]
陈雪冬 [1]
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航空动力学报 [2]
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Creator:王发民
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Document Type:期刊论文
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钝化前缘乘波布局及其一体化构型气动特性
期刊论文
航空动力学报, 2013, 卷号: 28, 期号: 2, 页码: 379-384
Authors:
陈雪冬
;
王发民
Adobe PDF(1058Kb)
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Submit date:2013/03/07
钝化前缘
高超声速
乘波布局
一体化构型
气动特性
高超声速进气道起动特性数值研究
期刊论文
宇航学报, 2007, 卷号: 28, 期号: 6, 页码: 1482-1487
Authors:
丁海河
;
王发民
Adobe PDF(791Kb)
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View/Download:571/177
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Submit date:2010/05/03
进气道
起动特性
边界层抽吸
高超声速飞行器-进气道一体化热流数值计算
期刊论文
航空动力学报, 2007, 卷号: 22, 期号: 8, 页码: 1297-1302
Authors:
丁海河
;
王发民
Adobe PDF(403Kb)
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Submit date:2010/05/03
航空、航天推进系统
气动热
超燃冲压发动机
转捩
Cfd(计算流体动力学)
乘波飞行器构型方法研究
期刊论文
力学学报, 2004, 卷号: 36, 期号: 5, 页码: 513-519
Authors:
王发民
;
李立伟
;
姚文秀
;
雷麦芳
Adobe PDF(559Kb)
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Submit date:2007/06/15
乘波飞行器
变楔角楔/椭圆锥乘波体
气动力
升阻比
乘波前体构型设计与压缩性能分析
期刊论文
工程力学, 2003, 卷号: 20, 期号: 6, 页码: 130-134
Authors:
刘嘉
;
王发民
Adobe PDF(192Kb)
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View/Download:542/141
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Submit date:2010/05/03
乘波体
相交楔锥
压缩性
一体化设计