關鍵字查詢 | 類別:會議論文 | | 關鍵字:Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated Airfoil

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序號 學年期 教師動態
1 99/2 航太系 洪健君 副教授 會議論文 發佈 Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated Airfoil , [99-2] :Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated Airfoil會議論文Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated AirfoilSun, W.-H; Miao, J-.M; Tai, C.-H; Hung, C.-C.MAVs;aerodynamic,;ANOVA analysis; vorticityMY74000The development of biomimetic micro-aerial-vehicles (MAVs) with flapping wings is the future trend in military/domestic field. The successful flight of MAVs is strongly related to the understanding of unsteady aerodynamic performance of low Reynolds number airfoils under dynamic flapping motion. This study explored the effects of flapping frequency, stroke amplitude, and the inclined angle of stroke plane on lift force and thrust force of a bio-inspiration corrugated airfoil with 33 full factorial design of experiment and ANOVA analysis. Unsteady vorticity flows over a corrugated thin airfoil executing flapping motion are computed with time-dependent two-dimensional laminar incompressible Reynolds-averaged Navier-S
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