TY - GEN
T1 - Scalar conservation in large eddy simulations of reacting flows
AU - Subbareddy, Pramod K
AU - Candler, Graham V.
AU - Ferrero, Pietro
PY - 2014
Y1 - 2014
N2 - Large eddy simulation is the most viable approach for the accurate simulation of turbulent reacting flows. With the proper combination of high-order, low-dissipation numerical methods, physics-based subgrid-scale models, and boundary conditions it is becoming possible to simulate many combustion flows at relevant conditions. However, non-premixed flows are a particular challenge because the thickness of the fuel/oxidizer interface scales inversely with Reynolds number. Most numerical methods diffuse the interface, resulting in artificial mixing and spurious reactions. Furthermore, when higher-order numerical methods are used, there are often aphysical undershoots and overshoots in the scalar variables (e.g. species mass fractions or progress variable). In this paper, we attempt to construct a numerical method that mitigates this issue.
AB - Large eddy simulation is the most viable approach for the accurate simulation of turbulent reacting flows. With the proper combination of high-order, low-dissipation numerical methods, physics-based subgrid-scale models, and boundary conditions it is becoming possible to simulate many combustion flows at relevant conditions. However, non-premixed flows are a particular challenge because the thickness of the fuel/oxidizer interface scales inversely with Reynolds number. Most numerical methods diffuse the interface, resulting in artificial mixing and spurious reactions. Furthermore, when higher-order numerical methods are used, there are often aphysical undershoots and overshoots in the scalar variables (e.g. species mass fractions or progress variable). In this paper, we attempt to construct a numerical method that mitigates this issue.
UR - http://www.scopus.com/inward/record.url?scp=85087190162&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85087190162&partnerID=8YFLogxK
U2 - 10.2514/6.2014-3203
DO - 10.2514/6.2014-3203
M3 - Conference contribution
AN - SCOPUS:85087190162
SN - 9781624102936
T3 - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference
BT - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference 2014
Y2 - 16 June 2014 through 20 June 2014
ER -