论文信息 - An overview of micro air vehicle aerodynamics

An overview of micro air vehicle aerodynamics

Nomenclature AR = full-span aspect ratio, b/S b = wingspan CD = drag coefficient (three-dimensional) Cd = section drag coefficient Cf = skin friction coefficient CL = lift coefficient (three-dimensional) Q = section lift coefficient CL I CD = endurance parameter Ci/Cd = section lift-to-drag ratio c = root-chord length Rec = root-chord Reynolds number S = wing area t = wing thickness a = angle of attack

Thomas J. Mueller | T. Mueller

[1] I. E. Garrick. Propulsion of a flapping and oscillating airfoil , 1936 .

[2] Thomas J. Mueller,et al. Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers , 2001 .

[3] M. L. Henderson,et al. Low-speed single-element airfoil synthesis , 1979 .

[4] Jerzy Maryniak. LONGITUDINAL STABILITY OF A GLIDER IN RIGID TOW , 1972 .

[5] Geoffrey Spedding,et al. The Aerodynamics of Flight , 1992 .

[6] Franz Villinger,et al. Man Powered Flight in 1929 , 1960 .

[7] J. Rayner. A vortex theory of animal flight. Part 2. The forward flight of birds , 1979, Journal of Fluid Mechanics.

[8] T. Weis-Fogh. Unusual mechanisms for the generation of lift in flying animals. , 1975, Scientific American.