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Two computational approaches (DNS and LES/PDF) for simulating turbulent combustion Realistic treatment of complex fuel chemistry Overview Computer simulations essential to the development and optimization of new combustion technologies Transportation (automotive, trucks, aircraft, …) Power generation Future transportation fuels From biomass, coal, … Oxygenated hydrocarbons Different combustion properties Motivation Resolve all length and time scales Detailed chemistry and material properties No modeling Massive computations Restricted to small, simple geometries Provides understanding of processes, test cases for models Direct Numerical Simulation (DNS) Resolve only large scales Model turbulence-chemistry interactions Applicable in engineering design Large-eddy Simulation (LES)/Probability Density Function (PDF) DNS of a Turbulent Lifted Ethylene/air Jet Flame LES/PDF of a Turbulent Lifted H 2 /N 2 Jet Flame Office of Science C 2 H 4 /N 2 (550K) air (1550K) air (1550K) 2D scatter plot of the particle locations, colored by temperature at t = 2 j Excellent agreement between LES/PDF results and Exp. data Promising design tool for engineering applications Makes excellent use of exa-scale computations Yields valuable insights into the small scale interactions Comparative studies with DNS and LES/PDF Apply the computer simulation tools to oxygenated fuels Future Work May 2527, 2011 Washington, D.C. Cylinder domain [0 230]x[0 90]x[0 2π] (unit: mm) Mesh size 216×144×96 ~ 3M Computational cost 0.5 million CPU hours Box domain [0 30]x[[0 40]x[0 6] (unit: mm) Mesh size 2025x1600x400 ~ 1.3G Computational cost 14 million CPU hours Cabra et al. (2002) (Cabra et al., 2002) Volume rendering of scalar dissipation rate, mixture fraction, mass fraction of HO 2 , CH 3 , and OH in the lifted ethylene jet flame. Visualization by K. L. Ma at UC Davis and H. Yu at SNL. log HO 2 CH 3 OH ACKNOWEDGMENT: This work is supported as part of the Combustion Energy Frontier Research Center funded by the US Department of Energy, Office of Science, Office of Basic Energy Sciences under Award Number DE-SC0001198. Computational resources are provided through DOE INCITE program.

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Two computational approaches (DNS and LES/PDF) for

simulating turbulent combustion

Realistic treatment of complex fuel chemistry

Overview

Computer simulations essential to the development and

optimization of new combustion technologies

Transportation (automotive, trucks, aircraft, …)

Power generation

Future transportation fuels

From biomass, coal, …

Oxygenated hydrocarbons

Different combustion properties

Motivation

Resolve all length and time scales

Detailed chemistry and material properties

No modeling

Massive computations

Restricted to small, simple geometries

Provides understanding of processes, test cases for models

Direct Numerical Simulation (DNS)

Resolve only large scales

Model turbulence-chemistry interactions

Applicable in engineering design

Large-eddy Simulation (LES)/Probability Density

Function (PDF)

DNS of a Turbulent Lifted Ethylene/air Jet Flame

LES/PDF of a Turbulent Lifted H2/N2 Jet Flame

Office of

Science

C2H4/N2

(550K)

air

(1550K)air

(1550K) 2D scatter plot of the particle locations, colored by temperature at t = 2j

Excellent agreement between LES/PDF results and Exp. data

Promising design tool for engineering applications

Makes excellent use of exa-scale computations

Yields valuable insights into the small scale interactions

Comparative studies with DNS and LES/PDF

Apply the computer simulation tools to oxygenated fuels

Future Work

May 25—27, 2011

Washington, D.C.

Cylinder domain [0 230]x[0 90]x[0 2π] (unit: mm)

Mesh size 216×144×96 ~ 3M

Computational cost 0.5 million CPU hours

Box domain [0 30]x[[0 40]x[0 6] (unit: mm)

Mesh size 2025x1600x400 ~ 1.3G

Computational cost 14 million CPU hours

Cabra et al. (2002)

(Cabra et al., 2002)

Volume rendering of scalar dissipation rate, mixture fraction, mass fraction of HO2, CH3, and OH in the lifted

ethylene jet flame. Visualization by K. L. Ma at UC Davis and H. Yu at SNL.

log HO2 CH3 OH

ACKNOWEDGMENT: This work is supported as part of the Combustion Energy Frontier Research Center funded by the US

Department of Energy, Office of Science, Office of Basic Energy Sciences under Award Number DE-SC0001198. Computational

resources are provided through DOE INCITE program.