Comb Wings For Flapping Flight At Extremely Low Reynolds Numbers

d = distance between two adjacent bodies within the row e = ellipsoid eccentricity l = rod half-length m = number of rods within a row p = pressure s = a point along the rods axis u = velocity vector u; v; w = components of velocity in the normal, n, tangential, s, and binormal, b, directions respectively ji s , j i s = intensities of Stokeslets and doublets at point s = slenderness ratio of an individual rod = dynamical viscosity = density