Research Papers: Gas Turbines: Combustion, Fuels, and Emissions

NO Prediction in Turbulent Diffusion Flame Using Multiple Unsteady Laminar Flamelet Modeling

[+] Author and Article Information
Rakesh Yadav

34/1, Rajiv Gandhi Infotech Park,
Pune 411057,India
e-mail: rakesh.yadav@ansys.com

Pravin Nakod

34/1, Rajiv Gandhi Infotech Park,
Pune 411057, India
e-mail: pravin.nakod@ansys.com

Pravin Rajeshirke

34/1, Rajiv Gandhi Infotech Park,
Pune 411057, India
e-mail: pravin.rajeshirke@ansys.com

Manuscript received January 11, 2014; final manuscript received February 2, 2014; published online May 9, 2014. Editor: David Wisler.

J. Eng. Gas Turbines Power 136(10), 101515 (May 09, 2014) (9 pages) Paper No: GTP-14-1022; doi: 10.1115/1.4026801 History: Received January 11, 2014; Revised February 02, 2014

The steady laminar flamelet model (SLFM) (Peters, 1984, “Laminar Diffusion Flamelet Models in Non-Premixed Turbulent Combustion,” Prog. Energy Combust. Sci., 10(3), pp. 319–339; Peters, 1986, “Laminar Flamelet Concepts in Turbulent Combustion,” Symp. (Int.) Combust., 21(1), pp. 1231–1250) has been shown to be reasonably good for the predictions of mean temperature and the major species in turbulent flames (Borghi, 1988, “Turbulent Combustion Modeling,” Prog. Energy Combust. Sci., 14(4), pp. 245–292; Veynante and Vervisch, 2002, “Turbulent Combustion Modeling,” Prog. Energy Combust. Sci., 28(3), pp. 193–266). However, the SLFM approach has limitations in the prediction of slow chemistry phenomena like NO formation (Benim and Syed, 1998, “Laminar Flamelet Modeling of Turbulent Premixed Combustion,” Appl. Math. Model., 22(1–2), pp. 113–136; Heyl and Bockhorn, 2001, “Flamelet Modeling of NO Formation in Laminar and Turbulent Diffusion Flames,” Chemosphere, 42(5–7), pp. 449–462). In the case of SLFM, the turbulence and chemistry are coupled through a single variable called scalar dissipation, which is representative of the strain inside the flow. The SLFM is not able to respond to the steep changes in the scalar dissipation values and generally tends to approach to the equilibrium solution as the strain relaxes (Haworth et al., 1989, “The Importance of Time-Dependent Flame Structures in Stretched Laminar Flamelet Models for Turbulent Jet Diffusion Flames,” Symp. (Int.) Combust., 22(1), pp. 589–597). A pollutant like NO is formed in the post flame zones and with a high residence time, where the scalar dissipation diminishes and hence the NO is overpredicted using the SLFM approach. In order to improve the prediction of slow forming species, a transient history of the scalar dissipation evolution is required. In this work, a multiple unsteady laminar flamelet approach is implemented and used to model the NO formation in two turbulent diffusion flames using detailed chemistry. In this approach, multiple unsteady flamelet equations are solved, where each flamelet is associated with its own scalar dissipation history. The time averaged mean variables are calculated from weighted average contributions from different flamelets. The unsteady laminar flamelet solution starts with a converged solution obtained from the steady laminar flamelet modeling approach. The unsteady flamelet equations are, therefore, solved as a post processing step with the frozen flow field. The domain averaged scalar dissipation for a flamelet at each time step is obtained by solving a scalar transport equation, which represents the probability of occurrence of the considered flamelet. The present work involves the study of the effect of the number of flamelets and also the different methods of probability initialization on the accuracy of NO prediction. The current model predictions are compared with the experimental data. It is seen that the NO predictions improves significantly even with a single unsteady flamelet and further improves marginally with an increase in number of unsteady flamelets.

Copyright © 2014 by ASME
Your Session has timed out. Please sign back in to continue.



Grahic Jump Location
Fig. 2

Schematic of the burner of Delft III Flame [18]

Grahic Jump Location
Fig. 1

Schematic and computational domain for SFD [17]

Grahic Jump Location
Fig. 3

Axial profile of temperature and species mass fractions at centerline for SFD using SLFM

Grahic Jump Location
Fig. 4

Axial profiles of species mass fraction at centerline using single unsteady flamelet with different initialization of unsteady flamelet

Grahic Jump Location
Fig. 5

Contours of initial probability for different flamelets for one, three, and six unsteady flamelets cases

Grahic Jump Location
Fig. 6

Scalar dissipation histories and integral of unsteady flamelet probabilities with (a) one, (b) three, and (c) six unsteady flamelets

Grahic Jump Location
Fig. 7

Primary air inlet boundary conditions profiles for Delft Flame III

Grahic Jump Location
Fig. 8

Fuel inlet boundary conditions profiles for Delft Flame III

Grahic Jump Location
Fig. 9

Radial profiles of flow variables and species mass fractions at two axial location of x = 100 and 200 mm from the fuel jet exit for Delft Flame III

Grahic Jump Location
Fig. 10

Radial profiles of species mass fractions at 100 and 200 mm away from fuel jet with single unsteady flamelet

Grahic Jump Location
Fig. 11

Initialization of the different flamelets for multiple unsteady flamelets for Delft III flame (flamelet index is from right to left, similar to Fig. 5)

Grahic Jump Location
Fig. 12

Scalar dissipation histories with different number of flamelets for Delft Flame III

Grahic Jump Location
Fig. 13

Effect of number of flamelets on NO prediction




Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In