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Abstrakty
In the present work, the large eddy simulation (LES) has been used to simulate a single fuel jet reacting flow under the conditions of highly preheated and diluted air combustion (HPDAC). A hybrid procedure of the standard subgrid scale (SGS) magorinky-Lille model and Reynolds stress model (RSM) together with the finite rate/eddy dissipation reaction model has been employed to simulate a single wall jet HPDAC furnace chamber. The propane-air two-step combustion system is selected for modeling under two different HPDAC inlet air conditions corresponding to 3% w/w oxygen at 1300K and 21% w/w oxygen at 1300K. The numerical results show that the standart Smagorinsky model and Reynolds stress model together with the finite rate/eddy disspation model are capable of predicting the global flame effects on the flow, such as flow velocities, mixing patterns, temperatures and turbulent parameters. The predictions are found in acceptable agreement with the corresponding results of in-furnace measurements and physical modeling. By compared with the pure Reynolds stress model, it is found that the differences between the two predictions of LES and RSM are insignificant in the near field of the flow. The Smagorinsky constant C, has been also tuned in the work. It illustrates that Cs value significantly influences the predictions on both near field and far of the jet flow. Though, further development of SGS stress and combustion models is needed, it is found that LES is an attratctive tool to simulate the dynamic processes of turbulent reacting flows for the HPDAC furnaces.
Czasopismo
Rocznik
Tom
Strony
163--176
Opis fizyczny
Bibliogr. 29 poz., rys.
Twórcy
autor
- Division of Heat and Furnace Technology, Royal Institute of Technology Stockholm, Sweden
autor
- Division of Heat and Furnace Technology, Royal Institute of Technology Stockholm, Sweden
Bibliografia
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- [2] LAUNDER, B.E.: Second-Moment Closure: Present...and Future? International Journal of Heat Fluid Flow, 10 (4), (1989), pp. 282-300.
- [3] LILLY D.K.: On the application of the eddy viscosity concept in the intertial subrange of turbulence. NCAR Manuscript 123, (1966).
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- [5] PlOMELLI U., Liu J.: Large-eddy simulation of rotating channel flows using a localized dynamic model. Phys. Fluids, 7, (1995), pp. 839-848.
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- [7] OLSSON M.: Large eddy simulation of turbulent jets. Doctoral thesis, Royal Institute of Technology, Stockholm, Sweden, (1997).
- [8] COOK A.W., RILEY J.J.: Combust. Flame 109, (1997), pp. 332-341; 112, (1998), pp. 593-606.
- [9] LIBBY P.A., WILLIAMS F.A.: Turbulent reacting flows. Academic, New York, 1994.
- [10] BUTLER T.D., O'ROURKE P.J.: In 16th Symp.(Int.) on Combustion, (1977), pp. 1503-1515.
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- [13] BOGER M.: In 27th Symposium (international) on Combustion, (1998), pp. 917-925.
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- [15] GAO F., O'BRIEN E.E.: Phys. Fluids A, 5, (1988), pp. 1282-1284.
- [16] FRANKEL S.H.: Engineering applications of large eddy simulations, Fluid Engineering Division, ASME, 162, (1993), pp.81-101.
- [17] DESJARDIN P.E., FRANKEL S.H.: Large eddy simulation of a non-premixed reacting jet: Application and assessment of subgrid-scale combustion models. Phys. Fluids, 10, 9, (1998), 2298-2314.
- [18] MAGNUSSEN B.F., HJERTAGER B.H.: On mathematical models of turbulent combustion with special emphasis on soot formation and combustion. Technical report, 16th Symp. (Int'1.) on Combustion, Cambridge, MA, Aug. 15-20, (1976).
- [19] BAI X.S., FUCHS L., GULLBRAND J.: On modeling aspects of swirling stabilized diffusion fames. AIAA 97-0371,(1997).
- [20] GULLBRAND J., BAI X.S., FUCHS L.: Large eddy simulation of turbulent reacting flows using Cartesian grid and boundary corrections. AIAA, 98-3317, (1998).
- [21] SMAGORINSKY J.: General circulation experiments with the primitive equations. I. The Basic Experiment. Month. Wea. Rev., 91, (1963), pp. 99-164.
- [22] LILLY D.K.: On the application of the eddy viscosity concept in the intertial subrange of turbulence. NCAR Manuscript 123, (1966).
- [23] SPALDING D.B.: Mixing and chemical reaction in steady confined turbulent flames. In 13th Symp. (Int'1.) on Combustion, The Combustion Institute, (1970).
- [24] PATANKAR S.V.: Numerical heat transfer and fluid flow. Hemisphere, Washington, D.C., (1980).
- [25] HUTCHINSON B.R., RAITHBY G.D.: A multigrid method based on the additive correction strategy. Numerical Heat Transfer, 9, (1986), pp. 511-537.
- [26] LILLE S.: Experimental study of single fuel jet in conditions of highly preheated air combustion. Licentiate thesis. Royal Institute of Technology, Stockholm, Sweden, (1999).
- [27] OLSSON H.: Highly diluted and preheated oxidation. Licentiate thesis. Royal Institute of Technology, Stockholm, Sweden, (1999).
- [28] DONG W.: Design of Advanced Industrial Furnaces Using Numerical Modeling Method. Ph.D. thesis, Royal Instittue of Technology, Stockholm, Sweden, (2000).
- [29] SCHMIDT H., SCHUMANN U.: Coherent structure of the convective boundary layer derived from large-eddy simulations. J. Fluid Mech., 200, (1989), pp. 511-562.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWM2-0009-0022
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