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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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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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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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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)
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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)
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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)
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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)
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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)
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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)
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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)
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Hypersonic flow  Shock wave/turbulent boundary-layer interactions  Thermochemical non-equilibrium  Turbulence model