中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共6条，第1-6条 帮助

限定条件                
已选(0)清除 条数/页：   排序方式：
Estimating forces from cross-sectional data in the wake of flows past a plate using theoretical and data-driven models 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 19
作者:  Tong, Wenwen;  Wang SZ(王士召);  Yang, Yue
Adobe PDF(4063Kb)  |  收藏  |  浏览/下载：140/20  |  提交时间：2022/12/20
Optimal reduced frequency for the power efficiency of a flat plate gliding with spanwise oscillations 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 11, 页码: 111908
作者:  Wang CY(王春雨);  Zhao Y(昭越);  Zhang XL(张鑫磊);  Wang SZ(王士召)
Adobe PDF(9166Kb)  |  收藏  |  浏览/下载：121/23  |  提交时间：2022/10/25
Predicting the near-wall velocity of wall turbulence using a neural network for particle image velocimetry 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 115105
作者:  Wang HP(王洪平);  Yang ZX(杨子轩);  Li BL(李秉霖);  Wang SZ(王士召)
Adobe PDF(5162Kb)  |  收藏  |  浏览/下载：361/111  |  提交时间：2020/12/28
CHANNEL FLOW  BOUNDARY-LAYER  FRICTION  MODEL  GENERATION  DATABASE  REGION  
Characterizing three-dimensional features of vortex surfaces in the flow past a finite plate 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 1, 页码: 15
作者:  Tong WW;  Yang Y(杨越);  Wang SZ(王士召)
Adobe PDF(6216Kb)  |  收藏  |  浏览/下载：262/97  |  提交时间：2020/05/18
Lift enhancement by dynamically changing wingspan in forward flapping flight 期刊论文
PHYSICS OF FLUIDS, 2014, 卷号: 26, 期号: 6, 页码: 61903
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2410Kb)  |  收藏  |  浏览/下载：784/179  |  提交时间：2014/11/03
Immersed Boundary Method  Leading-edge Vortices  Insect Flight  Aerodynamic Performance  Unsteady Aerodynamics  Wake Structure  Free Vortex  Bat Flight  Kinematics  Flow  
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：875/372  |  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