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- W2385067609 abstract "Numerical computations for Micro Aerial Vehicle(MAV) applications were conducted to analyze the effects of airfoil relative thickness and its position to dynamic aerodynamic characteristics of airfoil with identical pitching rate at low Reynolds number.The dual-step Roe schema developed by Rogers was used to solve the incompressible Navier-Stokes equations revised by artificial compressibility method.Verification was done between the numerical results and Walker's experimental results.Taken the length of airfoil chord as the characteristic length,at the low Reynolds number(Re=500,5000 and 50000),the dynamic aerodynamic characteristics were researched about different values of maximum relative thickness and position.The research results indicated that the effect of the former is more obvious than the latter,and the greater maximum relative thickness leads to the larger dynamic lift-drag ratio." @default.
- W2385067609 created "2016-06-24" @default.
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- W2385067609 date "2008-01-01" @default.
- W2385067609 modified "2023-09-23" @default.
- W2385067609 title "The effect of relative thickness to the dynamic aerodynamic characteristics about pitching airfoils" @default.
- W2385067609 hasPublicationYear "2008" @default.
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