Force and moment on a Joukowski profile in the presence of point vortices

OR many purposes, inviscid flow simulation by means of twodimensional potential flow theory and point vortices provides valuable information about unsteady flow over high-aspect-ratio wings.1'2 One way of calculating the flowfield and vortex convection velocities is to represent the foil shape as a conformal mapping of a circle, making use of the powerful theory of functions of a complex variable.3"5 The wake of the profile is discretized into point vortices, and the circle theorem insures that the body boundary condition is satisfied everywhere on the foil. Assuming that the Kutta condition of finite flow velocity at the trailing edge holds,6 new vortices of the appropriate strength are continually released in the wake. An algorithm for time integration is all that is needed to complete the simulation of large-amplitu de foil motion. In cases where the exact profile shape is of secondary importance, a Joukowski mapping can be used, and the resulting expressions for the complex potential become particularly simple.7"11 We show that the force and moment acting on the Joukowski profile throughout the simulation consist of added mass terms as if the flow were free of vortices plus the summed effect of all of the vortices in the flow.

[1]  Michael S. Triantafyllou,et al.  Efficient Foil Propulsion Through Vortex Control , 1996 .

[2]  Dean T. Mook,et al.  Perspective: Numerical Simulations of Wakes and Blade-Vortex Interaction , 1994 .

[3]  T. Tavares,et al.  Perspective: Unsteady Wing Theory—The Kármán/Sears Legacy , 1993 .

[4]  G. Choksi,et al.  Numerical Simulation of the Unsteady Wake Behind an Airfoil , 1989 .

[5]  D. H. Choi,et al.  Inviscid Analysis of Two-Dimensional Airfoils in Unsteady Motion , 1988 .

[6]  L. Greengard,et al.  A Fast Adaptive Multipole Algorithm for Particle Simulations , 1988 .

[7]  Leslie Greengard,et al.  A fast algorithm for particle simulations , 1987 .

[8]  Chuen-Yen Chow,et al.  The initial lift and drag of an impulsively started airfoil of finite thickness , 1982, Journal of Fluid Mechanics.

[9]  J. M. R. Graham,et al.  The forces on sharp-edged cylinders in oscillatory flow at low Keulegan–Carpenter numbers , 1980, Journal of Fluid Mechanics.

[10]  G. Hancock,et al.  The unsteady motion of a two-dimensional aerofoil in incompressible inviscid flow , 1978, Journal of Fluid Mechanics.

[11]  J. S. Sheffield,et al.  Flow over a Wing with an Attached Free Vortex , 1977 .

[12]  Turgut Sarpkaya,et al.  An inviscid model of two-dimensional vortex shedding for transient and asymptotically steady separated flow over an inclined plate , 1975, Journal of Fluid Mechanics.

[13]  R. Clements,et al.  An inviscid model of two-dimensional vortex shedding , 1973, Journal of Fluid Mechanics.

[14]  J. P. Giesing,et al.  Nonlinear two-dimensional unsteady potential flow with lift. , 1968 .

[15]  P. Libby,et al.  Two-dimensional Problems in Hydrodynamics and Aerodynamics , 1965 .

[16]  Knut Streitlien,et al.  A simulation procedure for vortex flow over an oscillating wing , 1994 .

[17]  F. T. Korsmeyer AN ORDER N ALGORITHM FOR THE SOLUTION OF THE BOUNDARY INTEGRAL EQUATIONS OF POTENTIAL FLOW , 1990 .

[18]  A. Panaras,et al.  Numerical Modeling of the Vortex/Airfoil Interaction , 1987 .