Computing unsteady shock waves for aeroacoustic applications

DOI10.2514/3.12203zbMath0813.76062OpenAlexW2036249493MaRDI QIDQ4317322

Kristine R. Meadows, Jay Casper, David A. Caughey

Publication date: 7 June 1995

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.12203

zbMATH Keywords

noise generationnumerical errorsupersonic jetnumerical flux formulasspurious entropy wavestencil biasing parametersthird-order essentially nonoscillatory scheme

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20)

Related Items (1)

Transmission of a slowly moving shock across a nonconservative interface

This page was built for publication: Computing unsteady shock waves for aeroacoustic applications