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Hybrid rans/les of supersonic turbulent boundary layer using compact interpolation method
Modi B.,
Published in American Institute of Aeronautics and Astronautics Inc, AIAA
2021
Pages: 1 - 12
Abstract
A hybrid RANS/LES framework is proposed to simulate a zero pressure gradient supersonic turbulent boundary layer over a flat plate. A delayed detached eddy simulation (DDES) framework is used. A non-zonal approach is used to transition between a SST k − ω RANS model and a compressible dynamic Smagorinsky model. A finite volume based flow solver using a sixth-order compact interpolation method is developed for the purpose. The numerical method is validated using a Mach 2 zero pressure gradient flat plate turbulent boundary layer simulation. © 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
About the journal
JournalData powered by TypesetAIAA Scitech 2021 Forum
PublisherData powered by TypesetAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISSN0001-1452
Impact Factor1.868
Open AccessNo
Citation Styleunsrt
Sherpa RoMEO Archiving PolicyGreen