TY - GEN
T1 - High-order large eddy simulation validation in HPCMP CREATE™ kestrel COFFE
AU - Holst, Kevin R.
AU - Bond, Ryan S.
AU - Glasby, Ryan S.
AU - Erwin, J. Taylor
AU - Stefanski, Douglas L.
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - Initial work has been done to develop a prototype large eddy simulation (LES) capability within the COFFE finite-element CFD solver, which is a component of HPCMP CREATE-AV Kestrel. The mathematical framework for the Favre-averaged Navier-Stokes equations is outlined, and four different methods for handling subgrid scale turbulence are discussed. Results from two test cases, the Taylor-Green vortex and tandem spheres at Re = 3, 900, are presented and discussed. The Taylor-Green vortex is a canonical case in LES that tests a solver’s ability to handle the turbulent kinetic energy cascade from large eddies to small vortices to dissipation, while the tandem spheres case assesses its capacity to model complex, unsteady, multi-scale flow at low Mach and Reynolds numbers.
AB - Initial work has been done to develop a prototype large eddy simulation (LES) capability within the COFFE finite-element CFD solver, which is a component of HPCMP CREATE-AV Kestrel. The mathematical framework for the Favre-averaged Navier-Stokes equations is outlined, and four different methods for handling subgrid scale turbulence are discussed. Results from two test cases, the Taylor-Green vortex and tandem spheres at Re = 3, 900, are presented and discussed. The Taylor-Green vortex is a canonical case in LES that tests a solver’s ability to handle the turbulent kinetic energy cascade from large eddies to small vortices to dissipation, while the tandem spheres case assesses its capacity to model complex, unsteady, multi-scale flow at low Mach and Reynolds numbers.
UR - http://www.scopus.com/inward/record.url?scp=85141634306&partnerID=8YFLogxK
U2 - 10.2514/6.2018-0781
DO - 10.2514/6.2018-0781
M3 - Conference contribution
AN - SCOPUS:85141634306
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -