Analysis of unsteady supersonic viscous flows by a shock-fitting technique
- 1 July 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 34 (7), 1428-1434
- https://doi.org/10.2514/3.13249
Abstract
An extension of Moretti's classical shock-fitting technique is proposed to solve complicated unsteady viscous flows. This version allows the automatic treatment of flow structures featuring triple points and shock interactions. A fitting of contact discontinuities has also been introduced for a number of problems. The fitting procedure is used with a Navier-Stokes solver based on the A scheme. Validation tests for selected cases are presentedKeywords
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