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Knowledge Management System of Institue of Mechanics, CAS
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基于 CO2 的飞行器降温减阻技术优化方法及特性
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
姚子康
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View/Download:145/5
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Submit date:2023/07/10
飞行器热管理,仿生分形结构,优化,CO2 射流,降温减阻
爆轰驱动发射技术及含能结构材料超高速碰撞力学响应
学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:
唐伟奇
Adobe PDF(8800Kb)
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Submit date:2022/06/28
爆轰驱动
二级轻气炮
内弹道
非晶合金
高熵合金
Strain Hardening in Graphene Foams under Shear
期刊论文
ACS OMEGA, 2021, 卷号: 6, 期号: 35, 页码: 22780-22790
Authors:
Yang T(杨田)
;
Wang C(王超)
;
Wu ZB(武作兵)
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Submit date:2021/11/01
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
航空煤油冲击射流流动与传热特性研究
学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:
杜蒙蒙
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Submit date:2021/06/03
航空煤油
冲击射流
传热特性
流动及结构参数
非定常特性
液滴自发旋转动力学研究—液体马达新策略
学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:
王占龙
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Submit date:2021/06/30
液体马达, 液滴, 自发旋转, 液态金属, 酸性溶液
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
Authors:
Zhang W
;
Wang S
;
Wang Q
;
Ju SJ(鞠胜军)
;
Yan C
Adobe PDF(2859Kb)
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Submit date:2021/02/09
Aerodynamic thermal
Opposing jets
Parametric sensitivity analysis
Uncertainty quantification
Analysis of Variance
Non-Intrusive Polynomial Chaos
On the flow characteristics in different carotid arteries
期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 10, 页码: 17
Authors:
Chen Y(陈与)
;
Yang XL(杨晓雷)
;
Iskander AJ
;
Wang P
Adobe PDF(29659Kb)
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Submit date:2020/11/30
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2023Kb)
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Submit date:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed