NASA NTRS · 19930034854
Adaptive remeshing for three-dimensional compressible flow computations
Abstract
A practical solution algorithm for steady 3D Euler flows is presented. This algorithm employs coupling of a surface triangulator, an automatic tetrahedral mesh generator, an unstructured grid flow solver, and an error estimation procedure. The performance of the method is illustrated using a shock interaction problem in high Mach number flow over a swept circular cylinder.
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Peraire, J., Peiro, J., Morgan, K.. 1992-12-01. Adaptive remeshing for three-dimensional compressible flow computations. https://ntrs.nasa.gov/citations/19930034854
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