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Analysis of Hypersonic Nozzles with Newton and Preconditioned Newton-GMRES Methods

机译:牛顿和预处理牛顿-GMRES方法对高超声速喷嘴的分析

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This study aims to obtain and analyze hypersonic flow solutions using both the well-known and reliable Newton method and a preconditioned Newton-GMRES method that aims to improve on the regular Newton-GMRES, achieving a degree of reliability closer to that of Newton's while decreasing computational times. Three dimensional Euler equations are used for the analysis. The main objectives of this study are to obtain hypersonic flow solutions through the usage of Newton and preconditioned Newton-GMRES methods and analyze these solutions to compare their performances, also testing the feasibility of the aforementioned preconditioner. While Newton-GMRES methods do not require the calculation of a Jacobian matrix, the calculation of one for the Newton method is done analytically.
机译:这项研究旨在使用众所周知且可靠的牛顿法和经过预处理的牛顿-GMRES方法获得和分析高超音速流动解决方案,该方法旨在改进常规牛顿-GMRES,并在降低的同时达到接近牛顿的可靠性。计算时间。使用三维欧拉方程进行分析。这项研究的主要目的是通过使用牛顿法和预处理的牛顿-GMRES方法获得高超音速流动解决方案,并分析这些解决方案以比较它们的性能,并测试上述预处理器的可行性。尽管牛顿-GMRES方法不需要计算雅可比矩阵,但牛顿方法的一个计算是通过解析完成的。

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