| Citation: | LI Zhan-ke, XU Ding-guo, NIU Wen. Investigation on aerodynamic characteristics of flexible wing with different flexibilities[J]. Journal of Aerospace Power, 2011, 26(1): 136-140.
|
| [1] |
Smith R W,Shyy W.Computation of unsteady laminar flow over a flexible two-dimensional membrane wing[J]. Physics of Fluids,1995,7(9):2175-2184.
|
| [2] |
Shyy W,Smith R.Computation of laminar flow and flexible structure interaction[M]//Hafez M,Oshima K.Comp- utational Fluid Dynamics Review.New York:John Wiley & Sons,1995:777-796.
|
| [3] |
Smith R,Shyy W.Computation of aerodynamic coefficients for a flexible membrane airfoil in turbulent flow:a comparison with classical theory[J].Physics of Fluids,1996,8(12):3346-3353.
|
| [4] |
Shyy W,Udaykumar H S,Rao M M,et al.Computational fluid dynamics with moving boundaries[M].Washington,DC:Taylor & Francis, 1996.
|
| [5] |
Shyy W.Computational modeling for fluid flow and interfacial transport[M].Amsterdam,The Netherlands:Elsevier,1994.
|
| [6] |
Lian Y,Shyy W,Haftka R T.Shape optimization of a membrane wing for micro air vehicles .AIAA 2003-0106,2003.
|
| [7] |
Ashley S.Palm-size spy plane[J].Mechanical Engineering,1998,12(2):1-11.
|
| [8] |
李彦华,石文蕊.微型飞行器对传统航空技术的挑战[J].国际航空,2000(5):41-44. LI Yanhua,SHI Wenrui.The challenge of micro-aircraft over traditional aeronautical technologies[J].International Aviation,2000(5):41-44.(in Chinese)
|
| [9] |
吴越.微型飞机何时飞向战场[J].机器人技术与应用,1998(3):17-19. WU Yue.When micro-aircraft fly to the battlefield[J].Robot Technique Application,1998(3):17-19.(in Chinese)
|
| [10] |
罗均,蒋蓁,程维明,等.国际上微型飞行器研究的进展及其关键技术[J].上海大学学报(自然科学版),2001,7(4):293-296. LUO Jun,JIANG Zhen,CHENG Weiming,et al.Progress in the study of micro aerial vehicle (MAV) and the key technologies[J].Journal of Shanghai University(Natural Science Edition),2001,7(4):293-296.(in Chinese)
|
| [11] |
McMasters J H,Henderson M L.Low-speed single-element airfoil synthesis .SEE N79-23889,1979.
|
| [12] |
Selig M S,Guglielmo J J,Broern A P,et al.Experiments on airfoils at low Reynolds numbers .AIAA-1996-0062,1996.
|
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