NASA NTRS · 19860057949
An LU implicit 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 LU 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.. 1986-06-01. An LU implicit scheme for high speed inlet analysis. https://ntrs.nasa.gov/citations/19860057949
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