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Vortex-induced energy loss of a mixed-flow waterjet pump under different operating conditions 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 9, 页码: 323064
Authors:  Kan, Kan;  Xu, Yuhang;  Xu, Hui;  Feng, Jiangang;  Yang ZX(杨子轩)
Adobe PDF(4285Kb)  |  Favorite  |  View/Download：44/0  |  Submit date：2023/07/17
Mixed-flow waterjet pump  Entropy production  Turbulence dissipation  Enstrophy transport  
A practical approach to flow field reconstruction with sparse or incomplete data through physics informed neural network 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 3, 页码: 322302
Authors:  Xu SF(许盛峰);  Sun ZX(孙振旭);  Huang RF(黄仁芳);  Guo DL(郭迪龙);  Yang GW(杨国伟);  Ju SJ(鞠胜军)
Adobe PDF(4793Kb)  |  Favorite  |  View/Download：79/5  |  Submit date：2023/04/20
Physics informed neural network  Flow field reconstruction  Particle image velocimetry  Cosine annealing algorithm  Experimental fluid dynamics  
Mechanotransduction of liver sinusoidal endothelial cells under varied mechanical stimuli 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 17
Authors:  Shu XY(舒芯钰);  Li N(李宁);  Wu Y(武亿);  Li W(李旺);  Zhang XY(张晓宇);  Li PW(李培文);  Lv DY(吕东媛);  Lv SQ(吕守芹);  Long M(龙勉)
Adobe PDF(1359Kb)  |  Favorite  |  View/Download：387/108  |  Submit date：2021/05/06
Liver sinusoidal endothelial cell  Shear stress  Mechanical stretch  Extracellular matrix  Stiffness  
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  Favorite  |  View/Download：398/63  |  Submit date：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:  Yao W(姚卫)
View  |  Adobe PDF(9586Kb)  |  Favorite  |  View/Download：656/295  |  Submit date：2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
DNS in evolution of vorticity and sign relationship in wake transition of a circular cylinder: (pure) mode A 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1131-1149
Authors:  Lin LM(林黎明);  Tan ZR
View  |  Adobe PDF(11593Kb)  |  Favorite  |  View/Download：290/50  |  Submit date：2019/12/17
Wake transition  Circular cylinder  Vorticity  Mode A  Sign law  
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1468Kb)  |  Favorite  |  View/Download：346/102  |  Submit date：2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
Mechanism of wavy vortex and sign laws in flow past a bluff body: vortex-induced vortex 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 1-14
Authors:  Lin LM(林黎明);  Shi SY(史仕荧);  Zhong XF(钟兴福);  Wu YX(吴应湘)
View  |  Adobe PDF(3794Kb)  |  Favorite  |  View/Download：431/72  |  Submit date：2019/04/11
Wavy vortex  Sign law  Vortex-induced vortex  Wake  Bluff body  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download：339/86  |  Submit date：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 4, 页码: 500-511
Authors:  Wu CK(吴承康);  Pan WX(潘文霞);  Meng X(孟显);  Wang, Hai-Xing;  Wu, CK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(878Kb)  |  Favorite  |  View/Download：458/129  |  Submit date：2015/10/21
Arc-heated Supersonic Jet  Low-power  Real Flow  Viscosity Effect  Low Reynolds Number