Large-eddy Simulation of Realistic Gas Turbine Combustors

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(a) (b) Figure 10: Instantaneous snapshot <strong>of</strong> temperature in the Pratt & Whitney combustor obtained from LES: a) symmetry plane with superimposed droplet locations, b) temperature contours at different cross-sections from the injector nozzle, the last plane represents the temperature measurement plane. 36
Page 1 and 2: Large-eddy Simulation of Realistic
Page 3 and 4: flows. In LES, three-dimensional, u
Page 5 and 6: in the continuity, Ṡ m , mixture
Page 7 and 8: 2.4 Liquid-Phase Equations The drop
Page 9 and 10: more width than height with deforma
Page 11 and 12: mass, d p = (6m p /πρ p ) 1/3 . T
Page 13 and 14: 3 Numerical Method A co-located, fi
Page 15 and 16: with sudden expansion. The primary
Page 17 and 18: through times. A convective boundar
Page 19 and 20: correctly represent the injector fl
Page 21 and 22: 5 Validation of Multi-physics React
Page 23 and 24: solver as well as the models used.
Page 25 and 26: [9] Apte, S. V., Mahesh, K., Moin,
Page 27 and 28: [30] Apte, S.V., Mahesh, K., and Lu
Page 29 and 30: 0.001 0.003 0.006 0.008 0.011 0.013
Page 31 and 32: 0.5 t=0.18 ms y, cm 0 -0.5 0 0.5 1
Page 33 and 34: y 6 4 2 0 (a) inlet wall outer swir
Page 35: Normalized Axial Mass Flowrate 8 6

Large-eddy Simulation of Realistic Gas Turbine Combustors

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