Engineering PapersSearch

NASA NTRS · 19830058186

Flux vector splitting and approximate Newton methods

Abstract

In the present investigation, the basic approach is employed to view an iterative scheme as Newton's method or as a modified Newton's method. Attention is given to various modified Newton methods which can arise from differencing schemes for the Euler equations. Flux vector splitting is considered as the basic spatial differencing technique. This technique is based on the partition of a flux vector into groups which have certain properties. The Euler equations fluxes can be split into two groups, the first group having a flux Jacobian with all positive eigenvalues, and the second group having a flux Jacobian with all negative eigenvalues. Flux vector splitting based on a velocity-sound speed split is considered along with the use of numerical techniques to analyze nonlinear systems, and the steady Euler equations for quasi-one-dimensional flow in a nozzle. Results are given for steady flows with shocks.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Jespersen, D. C., Pulliam, T. H.. 1983-01-01. Flux vector splitting and approximate Newton methods. https://ntrs.nasa.gov/citations/19830058186

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