Simulations of high-speed flow over an isolated roughness

Seokkwan Yoon, Michael D. Barnhardt, Graham V. Candler

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

21 Scopus citations

Abstract

A study has been performed to determine the feasibility of using computational fluid dynamics as a tool for predicting hypersonic boundary layer transition to turbulence and the resulting increase in heat transfer. Of particular interest is whether Detached Eddy Simulation can be used to overcome the scaling problems associated with Direct Numerical Simulation and Large Eddy Simulation of boundary layers. Fine-grid results for a boundary layer trip oriented 45 degrees to the flow inside a Mach 10 hypersonic wind tunnel show that Detached Eddy Simulation can predict transition in this perfect-gas flow.

Original languageEnglish (US)
Title of host publication48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
StatePublished - Dec 13 2010
Event48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: Jan 4 2010Jan 7 2010

Publication series

Name48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Other

Other48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
CountryUnited States
CityOrlando, FL
Period1/4/101/7/10

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