Saturation-free numerical scheme for computing the flow past a lattice of airfoils and the determination of separation points in a viscous fluid |
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Authors: | A G Petrov |
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Institution: | (1) Applied Aerodynamics Department, ONERA, 8 rue des Vertugadins - 92190, Meudon, France;(2) Computational Fluid Dynamics and Aeroacoustics Department, ONERA, BP 72 - 29, avenue de la Division Leclec - 92322, Chatillon, France;(3) Ecole Normale Superieure/LMD, 24 rue Lhomond - 75231, Paris cedex, 05, France |
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Abstract: | A numerical method for computing the potential flow past a lattice of airfoils is described. The problem is reduced to a linear
integrodifferential equation on the lattice contour, which is then approximated by a linear system of equations with the help
of specially derived quadrature formulas. The quadrature formulas exhibit exponential convergence in the number of points
on an airfoil and have a simple analytical form. Due to its fast convergence and high accuracy, the method can be used to
directly optimize the airfoils as based on any given integral characteristics. The shear stress distribution and the separation
points are determined from the velocity distribution at the airfoil boundary calculated by solving the boundary layer equations.
The method proposed is free of laborious grid generation procedures and does not involve difficulties associated with numerical
viscosity at high Reynolds numbers. |
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Keywords: | |
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