Search NASA⌕ Search

NASA NTRS · 19920053065

Finite element Euler calculations of unsteady transonic cascade flows

Abstract

A Galerkin finite element procedure incorporating an explicit Runge-Kutta time-stepping scheme has been developed in this work to solve unsteady transonic flow in cascades. The computational domain is discretized by a globally unstructured but locally structured blade-fitted deformable mesh. The Galerkin approximation is applied to the unsteady Euler equations based on a mixed Eulerian-Lagrangian description. The semi-discretized equations are integrated forward in time using a multistage Runge-Kutta scheme. An artificial dissipation operator of the type proposed by Jameson is adapted in the current scheme to capture shocks and suppress nonphysical oscillations. Phase-shifted boundary conditions are used to reduce the computational domain to a single reference passage. Results for both steady and unsteady transonic flows through cascades are presented and compared to existing finite volume solutions.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Hsiao, Chingteng, Bendiksen, Oddvar O.. 1992-01-01. Finite element Euler calculations of unsteady transonic cascade flows. https://ntrs.nasa.gov/citations/19920053065

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