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Engineering perspective on bird flight: Scaling, geometry, kinematics and aerodynamics 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 142, 页码: 47
作者:  Liu, Tianshu;  Wang SZ(王士召);  Liu, Hao;  He GW(何国威)
Adobe PDF(39199Kb)  |  收藏  |  浏览/下载：44/1  |  提交时间：2024/01/22
Bird  Flight  Scaling  Flapping wing  Airfoil  Wing geometry  Wing kinematics  Aerodynamics  Vortex  Lift  Drag  Thrust  Thin-airfoil theory  Lifting-line theory  Wake models  Kutta-Joukowski theorem  Actuator disk model  Vortex ring model  CFD  Multiple joint arm system  
Numerical simulation and scaling analysis of elasticity-induced lift force in a viscoelastic fluid between confining surfaces 期刊论文
JOURNAL OF HYDRODYNAMICS, 2022, 卷号: 34, 期号: 4, 页码: 756
作者:  Zhao X(赵欣);  Wei, Chao
Adobe PDF(2038Kb)  |  收藏  |  浏览/下载：126/36  |  提交时间：2022/10/23
Viscoelastic fluid  scaling expression  computational fluid dynamics  lift force  
Thermo-fluidic characteristics and performance in a distribute heating bubble pump generator 期刊论文
INTERNATIONAL JOURNAL OF REFRIGERATION, 2022, 卷号: 133, 页码: 181-190
作者:  Yang, Honghai;  Chen, Yuping;  Wu, Yiwei;  Yang FC(杨丰畅);  Huang, Xinyu;  Xu, Yue;  Duan, Wenli
Adobe PDF(1995Kb)  |  收藏  |  浏览/下载：190/45  |  提交时间：2022/02/17
Bubble pump generator  Distribute heating  Multiple lift tubes  Flow pattern evolution  Lift performance  Flow stability  
Particle manipulations in non-Newtonian microfluidics: A review 期刊论文
JOURNAL OF COLLOID AND INTERFACE SCIENCE, 2017, 卷号: 500, 页码: 182-201
作者:  Lu XY;  Liu C;  Hu GQ(胡国庆);  Xuan XC;  Xuan, XC (reprint author), Clemson Univ, Dept Mech Engn, Clemson, SC 29634 USA.
浏览  |  Adobe PDF(5915Kb)  |  收藏  |  浏览/下载：554/345  |  提交时间：2017/12/27
Elastic Lift  Inertial Lift  Particle Focusing  Particle Separation  Particle Washing  Particle Stretching  
High-Throughput Particle Manipulation Based on Hydrodynamic Effects in Microchannels 期刊论文
MICROMACHINES, 2017, 卷号: 8, 期号: 3
作者:  Liu C(刘超);  Hu GQ(胡国庆);  Hu, GQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing Key Lab Engn Construct & Mech, Beijing 100190, Peoples R China.;  Hu, GQ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(7127Kb)  |  收藏  |  浏览/下载：3259/2993  |  提交时间：2017/07/24
Particle Manipulation  Inertial Lift  Viscoelastic Effects  Microfluidics  Lab On a Chip  High Throughput  
A novel method of evaluating the lift force on the bluff body based on Noca's flux equation 期刊论文
CHINESE PHYSICS B, 2015, 卷号: 24, 期号: 8, 页码: 84701
作者:  Sui XK(隋相坤);  Jiang N(姜楠);  Sui, XK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(949Kb)  |  收藏  |  浏览/下载：236/84  |  提交时间：2016/01/08
Flux Equation  Lift Force  Experimental Error  
Tensionless contact of a finite beam: Concentrated load inside and outside the contact zone 期刊论文
Acta Mechanica Sinica, 2013, 卷号: 29, 期号: 6, 页码: 836-839
作者:  Zhang Y(张吟);  Murphy KD;  Zhang, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(873Kb)  |  收藏  |  浏览/下载：943/361  |  提交时间：2014/01/17
Tensionless Contact  Lift-off  Beam  
A lift formula applied to low-Reynolds-number unsteady flows 期刊论文
PHYSICS OF FLUIDS, 2013, 卷号: 25, 期号: 9, 页码: 093605/1-093605/22
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2214Kb)  |  收藏  |  浏览/下载：862/365  |  提交时间：2013/11/18
Reynolds Number  Acceleration Terms  Control Volumes  Flapping Wing  Inertial Effect  Lamb Vectors  Low Reynolds Number  Separated Flows  Unsteady Lift  
Tensionless contact of a finite circular plate 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1374-1381
作者:  Zhang Y(张吟);  Murphy KD;  Zhang, Y;  Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech LNM, Beijing 100190, Peoples R China.
Adobe PDF(425Kb)  |  收藏  |  浏览/下载：1249/668  |  提交时间：2013/01/18
Tensionless Contact  Elastic Foundation  Plate  Lift-off  Rectangular-plates  Half-space  Foundation  Adhesion  Beam  Supports  
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
作者:  Qi DW;  He GW(何国威);  Liu YM
Adobe PDF(738Kb)  |  收藏  |  浏览/下载：840/163  |  提交时间：2013/02/26
Aerospace Engineering  Deformation  Exhibitions  Flexible Wings  Reynolds Number  Rigidity  Vortex Flow  Aerodynamic Forces  Chord-based Reynolds Number  Flexural Rigidities  Free Stream  Free-stream Flow  Lattice Boltzmann  Leading-edge Vortices  Lift Coefficient  Lift Force  Particle Methods  Pitch Rate  Power Efficiency  Reduced Frequency  Three Dimensional Space  Time-periods  Tip Edge  Trailing Edges  Trailing Vortex