NASA NTRS · 19860014092
An LU implicity scheme for high speed inlet analysis
Abstract
A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The lower-upper implicit scheme in conjunction with adaptive dissipation proves to be an efficient and robust nonoscillatory shock capturing technique for high Mach number flows as well as for transonic flows.
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Yoon, S., Jameson, A.. 1986-04-01. An LU implicity scheme for high speed inlet analysis. https://ntrs.nasa.gov/citations/19860014092
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