Search NASA⌕ Search

NASA NTRS · 19900031087

Adaptive quadrilateral and triangular finite-element scheme for compressible flows

Abstract

The development of an adaptive mesh refinement procedure for analyzing high-speed compressible flows using the finite-element method is described. This new adaptation procedure, which uses both quadrilateral and triangular elements, was implemented with two explicit finite-element algorithms - the two-step Taylor-Galerkin and the multistep Galerkin-Runge-Kutta schemes. A von Neumann stability analysis and a rotating 'cosine hill'problem demonstrate the instability of the Taylor-Galerkin scheme when coupled with the adaptation procedure. For the same adaptive refinement scheme, the Galerkin-Runge-Kutta procedure yields stable solutions within its explicit stability limit. The utility of this new adaptation procedure for the prediction of compressible flow features is illustrated for inviscid problems involving strong shock interactions at hypersonic speeds.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Ramakrishnan, R., Thornton, Earl A., Bey, Kim S.. 1990-01-01. Adaptive quadrilateral and triangular finite-element scheme for compressible flows. https://ntrs.nasa.gov/citations/19900031087

Cite the original work for its findings. Save a collection to share your selection of sources.