NASA NTRS · 19880043339
Simple numerical method for solving the steady Euler equations
Abstract
A numerical method for solving the isenthalpic form of the governing equations for compressible inviscid flows is developed. The method is based on the concept of flux vector splitting in its implicit form and is tested on several demanding configurations. Time marching to steady state is accelerated by the implementation of the multigrid procedure which very effectively increases the rate of convergence. Steady-state results are obtained for various test cases. Only short computational times are required due to the relative efficiency of the basic method.
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Von Lavante, E., Melson, N. Duane. 1987-01-01. Simple numerical method for solving the steady Euler equations. https://ntrs.nasa.gov/citations/19880043339
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