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A collocation method for the generalized airfoil equation for an airfoil with a flap

机译:带有襟翼的翼型广义翼型方程的搭配方法

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摘要

We are concerned with the numerical solution of the generalized airfoil equation for an airfoil with a flap by means of global algebraic polynomial approximants. This problem has been considered in a recent paper by Monegato and Sloan [SIAM J. Numer. Anal., 34 (1997), pp. 2288-2305], where the authors proved the stability and convergence of a Galerkin method based on high order polynomials. They also presented very promising numerical results for the corresponding collocation method but left the theoretical results of stability and convergence as an open problem. We have succeeded in proving the stability and convergence properties of this collocation method by slightly modifying it in the neighborhood of the flap. The rate of convergence we have derived for our collocation method is very similar to that of the above Galerkin method. [References: 25]
机译:我们关注通过全局代数多项式近似对带有襟翼的翼型的广义翼型方程的数值解。 Monegato和Sloan [SIAM J. Numer。 Anal。,34(1997),pp。2288-2305],作者证明了基于高阶多项式的Galerkin方法的稳定性和收敛性。他们还为相应的配置方法提供了非常有希望的数值结果,但是将稳定性和收敛性的理论结果作为一个开放问题。通过在襟翼附近稍加修改,我们已经成功证明了这种搭配方法的稳定性和收敛性。我们为并置方法得出的收敛速度与上述Galerkin方法非常相似。 [参考:25]

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