NASA NTRS · 19890038146
Progress on a Taylor weak statement finite element algorithm for high-speed aerodynamic flows
Abstract
A new finite element numerical Computational Fluid Dynamics (CFD) algorithm has matured to the point of efficiently solving two-dimensional high speed real-gas compressible flow problems in generalized coordinates on modern vector computer systems. The algorithm employs a Taylor Weak Statement classical Galerkin formulation, a variably implicit Newton iteration, and a tensor matrix product factorization of the linear algebra Jacobian under a generalized coordinate transformation. Allowing for a general two-dimensional conservation law system, the algorithm has been exercised on the Euler and laminar forms of the Navier-Stokes equations. Real-gas fluid properties are admitted, and numerical results verify solution accuracy, efficiency, and stability over a range of test problem parameters.
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Baker, A. J., Freels, J. D.. 1989-01-01. Progress on a Taylor weak statement finite element algorithm for high-speed aerodynamic flows. https://ntrs.nasa.gov/citations/19890038146
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