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NASA NTRS · 19900031196

Finite element analysis of high speed compressible flows using mesh refinement/movement procedures

Abstract

An adaptive mesh refinement procedure for analyzing high-speed inviscid and viscous compressible flows is described. The adaptation procedure which uses both quadrilateral and triangular elements is implemented with an explicit finite element formulation. Elements in regions of strong and weak gradients are refined or coarsened based on inviscid and viscous indicators. Nodal locations are also adaptively moved to better resolve flow features. The effectiveness of the finite element procedure is demonstrated by modeling flows with complex shock structure and viscous-inviscid interactions. Numerical results are compared with experimental data.

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BibTeXRIS

Ramakrishnan, R., Thornton, E. A., Bey, K. S.. 1989-01-01. Finite element analysis of high speed compressible flows using mesh refinement/movement procedures. https://ntrs.nasa.gov/citations/19900031196

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