The Analysis of Aerodynamic Performance on the Flapping Wings
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 93 === A numerical method is developed to study the flapping wing flowfields. The method uses finite-volume method to solve the Euler equation. A diagonal dominant alternating direction implicit scheme (DDADI) coupling with an implicit residual smoothing is used...
Main Authors: | Shao-Fu Wang, 王少甫 |
---|---|
Other Authors: | San-Yih Lin |
Format: | Others |
Language: | zh-TW |
Published: |
2005
|
Online Access: | http://ndltd.ncl.edu.tw/handle/91176404150986268419 |
Similar Items
-
The Effects of Wing Design on the Aerodynamic Performance of a Flapping Wing
by: Guan-ying Jiang, et al.
Published: (2010) -
Effect of Wing Membrane Material on the Aerodynamic Performance of Flexible Flapping Wing
by: Lang, X., et al.
Published: (2022) -
Aerodynamic Analysis of a Flapping-Wing Micro Aerial Vehicle
by: Yu-Chun Fu, et al.
Published: (2007) -
Aerodynamics of Flapping Wings for Vertical Takeoff
by: G. C. Vishnu Kumar, et al.
Published: (2017-01-01) -
Numerical Investigation on Flapping Aerodynamic Performance of Dragonfly Wings in Crosswind
by: Chao Wang, et al.
Published: (2020-01-01)