Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-4 of 4 Help

Filters    
Selected(0)Clear Items/Page:    Sort:
Direct numerical simulations of hypersonic boundary layer transition over a hypersonic transition research vehicle model lifting body at different angles of attack 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 44111
Authors:  Men, Hongyuan;  Li XL(李新亮);  Liu HW(刘洪伟)
Adobe PDF(13263Kb)  |  Favorite  |  View/Download：50/6  |  Submit date：2023/06/15
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
Authors:  Tong WW;  Yang Y(杨越);  Wang SZ(王士召)
Adobe PDF(6216Kb)  |  Favorite  |  View/Download：291/103  |  Submit date：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
Authors:  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.
View  |  Adobe PDF(2410Kb)  |  Favorite  |  View/Download：806/187  |  Submit date：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
Authors:  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.
View  |  Adobe PDF(2214Kb)  |  Favorite  |  View/Download：897/379  |  Submit date：2013/11/18
Reynolds Number  Acceleration Terms  Control Volumes  Flapping Wing  Inertial Effect  Lamb Vectors  Low Reynolds Number  Separated Flows  Unsteady Lift