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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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Response characteristics and impact resistance of composite laminates with shear stiffening gel under hypervelocity impact
期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 219, 页码: 858-870./通讯作者:Zhang, Kun, Wei, Bingchen
Authors:
Liu ZS(刘子尚)
;
Jiang QY(姜泉宇)
;
Liu YZ(刘一哲)
;
Zhang K(张坤)
;
Wei YP(魏延鹏)
;
Chen TY(陈天宇)
;
Guo YC(郭雅悰)
;
Lu LL(路玲玲)
;
Wei BC(魏炳忱)
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View/Download:66/0
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Submit date:2024/06/17
Composite laminate
Shear stiffening gel
Vibration
Hypervelocity impact
Polyvinylidene fluoride
Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties
期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281./通讯作者:Lin, Xin, Wang, Zezhong
Authors:
Wang RY(王若岩)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Pan JJ(潘俊杰)
;
Zhang ZL(张泽林)
;
Luo JX(罗家枭)
;
Li F(李飞)
;
Yu XL(余西龙)
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Submit date:2024/05/21
Hybrid rocket
Composite fuel grain
Characteristic structure
Radiation image
Combustion properties
Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation
期刊论文
Acta Astronautica, 2024, 卷号: 216, 页码: 488-503./通讯作者:汪运鹏
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
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Submit date:2024/01/18
Multibody separation
Hypersonic
Dynamic stability
Center of pressure
Aerodynamic interaction
Numerical simulation
Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295./通讯作者:Wu, K
Authors:
Ao Y(敖彧)
;
Wu K(吴坤)
;
Lu, Hongbo
;
Ji, Feng
;
Fan XJ(范学军)
Adobe PDF(11339Kb)
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Submit date:2023/06/15
Hypervelocity combustion
Thermal nonequilibrium
Two-temperature model
Numerical simulation
Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113./通讯作者:Yue, LJ (corresponding author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
Authors:
He CM(何成明)
;
Zhang, Peng
;
He, Zhixia
;
Yue LJ(岳连捷)
Adobe PDF(20952Kb)
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Submit date:2023/04/20
Liquid rocket engine
Pintle injector
Spray characteristics
Jet film injection
Voronoi tessellation
An experimental investigation of supersonic combustion of cracked JP-10
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 203, 页码: 329-340./通讯作者:Zhang, Taichang
Authors:
Cui NF(崔乃夫)
;
Rao W(饶威)
;
Li YJ(李昱君)
;
Zhu, Yinhai
;
Zhang TC(张泰昌)
;
Fan XJ(范学军)
Adobe PDF(14542Kb)
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Submit date:2023/02/07
Cracking
JP-10
Supersonic combustion
Regenerative cooling
Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182./通讯作者:林鑫
Authors:
Zhang ZL(张泽林)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wu K(吴坤)
;
Luo JX(罗家枭)
;
Fang SH(方思晗)
;
Zhang CY(张春元)
;
Li F(李飞)
;
Yu XL(余西龙)
Adobe PDF(9227Kb)
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Submit date:2022/11/08
Hybrid rocket engine
Swirl injection
Novel composite fuel grain
Regression rate
Oxidizer-to-fuel ratio
Simplified analytical models for hypersonic lateral-directional stability
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 198, 页码: 431-444./通讯作者:Liu, W (corresponding author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Liu, W (corresponding author), Inst Mech, Beijing 100190, Peoples R China.
Authors:
Guo SQ(郭帅旗)
;
Liu W(刘文)
;
Zhang CA(张陈安)
;
Zhou X(周翔)
;
Wang FM(王发民)
Adobe PDF(6978Kb)
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Submit date:2022/10/23
Lateral stability
Directional stability
Analytical model
Viscous effects
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254./通讯作者:Sun, Bo
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(13791Kb)
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Submit date:2022/05/17
Mach 12 scramjet inlet
High temperature
Non-equilibrium effects
Thermochemical
Inlet performance
Thermochemical non-equilibrium effects on hypersonic shock wave/turbulent boundary-layer interaction
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 192, 页码: 1-14./通讯作者:Liu, Jun
Authors:
Jiang, Hao
;
Liu, Jun
;
Luo, Shichao
;
Huang, Wei
;
Wang, Junyuan
;
Liu MK(刘美宽)
Adobe PDF(9113Kb)
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Submit date:2022/05/17
Hypersonic flow
Shock wave/turbulent boundary-layer interactions
Thermochemical non-equilibrium
Turbulence model