NASA NTRS · 19890038148
An implicit and stiffly stable finite element CFD algorithm for unsteady aerodynamics
Abstract
A stable and accurate finite element CFD algorithm for hyperbolic/incompletely parabolic conservation law systems is described and verified. It combines a Taylor weak statement FEM, an optimal implicit Runge-Kutta time integration algorithm, and a matrix tensor product approximate factorization linear algebra procedure. The results of computational experiments show that the developed algorithm is robust.
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Baker, A. J., Iannelli, G. S.. 1989-01-01. An implicit and stiffly stable finite element CFD algorithm for unsteady aerodynamics. https://ntrs.nasa.gov/citations/19890038148
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