NASA NTRS · 19760003326
Inviscid transonic flow computations with shock fitting
Abstract
First-and second-order numerical procedures are presented for calculating two-dimensional transonic flows that treat shock waves as discontinuities. Their application to a simple but nontrivial problem for which there are limited theoretical results is discussed.
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Yu, N. J., Seebass, A. R.. 1975-01-01. Inviscid transonic flow computations with shock fitting. https://ntrs.nasa.gov/citations/19760003326
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