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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Han GL(韩桂来)
Favorite  |  View/Download：7/0  |  Submit date：2024/05/27
Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：57/8  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:  Yuan CK(苑朝凯);  Meng FZ(孟凡钊);  Liu, Xu;  Liu YF(刘云峰);  Lian H(连欢);  Liu, Yingzheng;  Peng, Di
Adobe PDF(3477Kb)  |  Favorite  |  View/Download：52/5  |  Submit date：2023/07/17
Temperature-sensitive paint  Heat flux  Conjugate gradient method  Air-breathing hypersonic vehicle  Inverse heat conduction problem  
Seal types of water-entry cavities generated by the impact of spheres with decreasing Bond number 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 6, 页码: 322482
Authors:  Zhong YX(钟玉雪);  Du Y(杜岩);  Qiu RD(丘润荻);  Xiao ZJ(肖志坚);  Huang J(黄荐);  Wang ZY(王志英);  Wang JZ(王静竹);  Wang YW(王一伟)
Adobe PDF(2740Kb)  |  Favorite  |  View/Download：59/5  |  Submit date：2023/07/17
Air cavity  Seal types  Laser-driven method  Shallow seal  Deep seal  
A computational method for the load spectra of large-scale structures with a data-driven learning algorithm 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 卷号: 66, 期号: 1, 页码: 141-154
Authors:  Chen XJ(陈贤佳);  Yuan, Zheng;  Li, Qiang;  Sun, ShouGuang;  Wei YJ(魏宇杰)
Adobe PDF(2512Kb)  |  Favorite  |  View/Download：293/87  |  Submit date：2023/02/09
load spectrum  computational mechanics  deep learning  data-driven modeling  gated recurrent unit neural network  
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：167/41  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
Recent Progress of Microgravity Science Research in China 期刊论文
空间科学学报, 2022, 卷号: 42, 期号: 4, 页码: 772-785
Authors:  Zhao JF(赵建福);  Du WF(杜王芳);  Kang Q(康琦);  Lan D(蓝鼎);  Li K(李凯);  Li WB(李伟斌);  Liu YC;  Luo XH;  Miao JY;  Wang QG;  Wang SF(王双峰);  Zhang T;  Zhang XW;  Zhang YH;  Zheng HQ
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A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3178Kb)  |  Favorite  |  View/Download：246/57  |  Submit date：2022/07/18
Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects  
Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  Favorite  |  View/Download：224/49  |  Submit date：2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency