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Rapid prediction of interface morphology and oxygen transportation in crystal growth based on the response surface method 期刊论文
JOURNAL OF CRYSTAL GROWTH, 2025, 卷号: 649, 页码: 9./通讯作者:Chen, Xue, Li, Kai
Authors:  Yan, Dongxiu;  Guo ZY(郭子漪);  Chen X(陈雪);  Li K(李凯);  Zhao JF(赵建福);  Hu WR(胡文瑞)
Favorite  |  View/Download:3/0  |  Submit date:2024/11/22
Crystal growth  Heat and mass flow  Interfacial phenomenon  Czochralski method  Kriging-based response surface method  
Anomalous size effect of impact resistance in carbon nanotube film 期刊论文
MATERIALS TODAY ADVANCES, 2024, 卷号: 24, 页码: 9./通讯作者:Xiao, Kailu, Hu, Dongmei, Wu, Xianqian
Authors:  Zhang, Wei;  Xiao KL(肖凯璐);  Hu, Dongmei;  Huang CG(黄晨光);  Wu XQ(吴先前)
Favorite  |  View/Download:30/0  |  Submit date:2024/11/01
Carbon nanotube films  Impact resistance  Size effect  Energy dissipation mechanisms  Failure mode  
Progress of Experimental Studies on Oblique Detonation Waves Induced by Hyper-Velocity Projectiles 期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 9, 页码: 21./通讯作者:Hu, Guotun, Wang, Qiu
Authors:  Shang JH(尚甲豪);  Hu, Guotun;  Wang Q(汪球);  Xiang, Gaoxiang;  Zhao W(赵伟)
Favorite  |  View/Download:9/0  |  Submit date:2024/11/01
oblique detonation wave  high-velocity launcher  non-intrusive measurement  initiation process  shock wave structure  
Kinetic Simulation of Nozzle Flow in a Micronewton-Class Cold Gas Thruster 期刊论文
AIAA JOURNAL, 2024, 页码: 10./通讯作者:Li, Yong, Hu, Yuan
Authors:  Sun WJ(孙文进);  Liu, Xuhui;  Long, Jun;  Wang, Xudong;  Sun QH(孙泉华);  Huang HJ(黄河激);  Li, Yong;  Hu Y(胡远)
Favorite  |  View/Download:38/0  |  Submit date:2024/10/08
Direct Simulation Monte Carlo  Micro Thruster  Variable Thrust  Multiscale Flow  Continuum Breakdown  
Study of Morphology of Gas-Liquid Interfaces in Tank with Central Column in CSS under Different Gravity Conditions 期刊论文
SYMMETRY-BASEL, 2024, 卷号: 16, 期号: 7, 页码: 21./通讯作者:Kang, Qi
Authors:  Chen ZW(陈哲文);  Duan L(段俐);  Chen ST(陈上通);  Li, Ce;  Yang C(杨超);  Hu L(胡良);  Zhang P(张璞);  Wu D(吴笛);  Zhang, Yuhao;  Pang, Huan;  Zhao YF(赵一凡);  Kang Q(康琦)
Favorite  |  View/Download:16/0  |  Submit date:2024/08/23
free surface  China Space Station  Young-Laplace equation  perturbation method  shooting method  different gravity conditions  
Static analysis and contact angle hysteresis study of bubbles in Chinese space station tank models under different gravity effects 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 7, 页码: 14./通讯作者:Kang, Qi
Authors:  Chen ZW(陈哲文);  Chen Y(陈一);  Wu D(吴笛);  Li, Ce;  Zhang, Yuhao;  Pang, Huan;  Duan L(段俐);  Wang J(王佳);  Ye ZJ(叶致君);  Zhang P(张璞);  Hu L(胡良);  Chen SY(陈舒扬);  Kang Q(康琦)
Favorite  |  View/Download:48/0  |  Submit date:2024/08/12
Study on Liquid Climbing Behavior During Filling Process in Tank Models Aboard the Chinese Space Station 期刊论文
MICROGRAVITY SCIENCE AND TECHNOLOGY, 2024, 卷号: 36, 期号: 4, 页码: 8
Authors:  Chen SY(陈舒扬);  Chen ST(陈上通);  Wu D(吴笛);  Duan L(段俐);  Liu, Xiaozhong;  Zhao, Xilin;  Zhang P(张璞);  Yang C(杨超);  Hu L(胡良);  Wang J(王佳);  Zhao YF(赵一凡);  Yin, Yongli;  Kang Q(康琦)
Favorite  |  View/Download:25/0  |  Submit date:2024/07/26
Plate type tank  Microgravity  Capillary driven flows  Chinese Space Station  
湿式离合器摩擦片表面油槽形式对带排扭矩及散热能力的影响 期刊论文
粉末冶金工业, 2024, 卷号: 34, 期号: 03, 页码: 54-59
Authors:  许成法;  张坤;  张登;  张国洪;  魏炳忱;  胡铮
Adobe PDF(2787Kb)  |  Favorite  |  View/Download:49/12  |  Submit date:2024/07/05
湿式离合器摩擦片  表面油槽  带排扭矩  散热能力  
Experimental study on the life and performance of an improved DC arc plasma torch 期刊论文
JOURNAL OF PHYSICS D-APPLIED PHYSICS, 2024, 卷号: 57, 期号: 20, 页码: 15./通讯作者:Sun, Su-Rong, Wang, Hai-Xing
Authors:  Hu YH(胡亚豪);  Sun, SuRong;  Meng X(孟显);  Huang HJ(黄河激);  Wang, HaiXing
Favorite  |  View/Download:113/0  |  Submit date:2024/04/02
DC arc plasma torch  shielding gas  nitrogen arc  electrode erosion  
Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units 期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18./通讯作者:Lin, Xin, Wang, Zezhong
Authors:  Pan JJ(潘俊杰);  Lin X(林鑫);  Wang ZZ(王泽众);  Wang RY(王若岩);  Wu K(吴坤);  Liang, Jinhu;  Yu XL(余西龙)
Favorite  |  View/Download:28/0  |  Submit date:2024/05/27
modular unit  modification  regression rate  combustion efficiency  hybrid rocket engine