Three-dimensional hypersonic boundary layer stability analysis with STABL-3D

Heath B. Johnson, Graham V. Candler, Christopher R. Alba

Research output: Chapter in Book/Report/Conference proceedingConference contribution

10 Scopus citations

Abstract

A suite of computer codes, developed at the University of Minnesota, for the analysis of reacting hypersonic boundary layer stability has been used successfully by many different researchers in a wide range of applications. However, these applications have been limited by the software to the analysis of axisymmetric or two-dimensional flows or to analysis in the symmetry planes of three-dimensional flows. This paper introduces the latest version of the software suite which has been extended for the analysis of three-dimensional flows. Comparisons are made with the already well-tested two-dimensional version of the codes, and results are presented to illustrate the new capabilities for analysis of three-dimensional flows.

Original languageEnglish (US)
Title of host publication40th AIAA Fluid Dynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781617389221
DOIs
StatePublished - 2010

Publication series

Name40th AIAA Fluid Dynamics Conference
Volume1

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