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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... [6]
Creator
王发民 [6]
刘宏 [4]
耿永兵 [4]
姚文秀 [2]
雷麦芳 [2]
康宏琳 [1]
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Journal ar... [6]
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2006 [5]
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中文 [5]
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力学学报 [2]
宇航学报 [2]
弹道学报 [1]
航空学报 [1]
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火箭增程乘波外形导弹弹道特性研究
期刊论文
弹道学报, 2006, 卷号: 18, 期号: 4, 页码: 1-3
Authors:
郭迪龙
;
张杰
;
康宏琳
;
王发民
Adobe PDF(144Kb)
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View/Download:736/184
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Submit date:2010/05/03
火箭增程
乘波外形
高超声速导弹
升阻比
弹道仿真
飞行高度及设计长度对锥形流乘波体优化的影响
期刊论文
宇航学报, 2006, 卷号: 27, 期号: 2, 页码: 162-166
Authors:
耿永兵
;
刘宏
;
王发民
Adobe PDF(287Kb)
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View/Download:518/195
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Submit date:2007/06/15
乘波体
优化设计
雷诺数
升阻比
锥形流乘波体优化设计研究
期刊论文
航空学报, 2006, 卷号: 27, 期号: 1, 页码: 23-28
Authors:
耿永兵
;
刘宏
;
姚文秀
;
王发民
Adobe PDF(328Kb)
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Submit date:2007/06/15
乘波体
优化设计
空气动力学
升阻比
高升阻比乘波构型优化设计
期刊论文
力学学报, 2006, 卷号: 38, 期号: 4, 页码: 540-546
Authors:
耿永兵
;
刘宏
;
雷麦芳
;
王发民
Adobe PDF(561Kb)
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Submit date:2007/06/15
乘波体
优化设计
气动力
升阻比
飞行高度及设计长度对锥形流乘波体优化的影响 Altitude and Design Length Effects of Optimized Waverider Derived from Cone Flow
期刊论文
宇航学报, 2006, 卷号: 27
Authors:
耿永兵
;
刘宏
;
王发民
Adobe PDF(371Kb)
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Submit date:2007/06/15
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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View/Download:732/242
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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