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Volumn , Issue , 2008, Pages 431-444

Numerical characterization of the non-reacting flow in a swirled gasturbine model combustor

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; NUMERICAL METHODS; TURBULENCE MODELS; TURBULENT FLOW; VELOCITY MEASUREMENT; VORTEX FLOW;

EID: 84892209745     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1007/978-3-540-74739-0_29     Document Type: Conference Paper
Times cited : (7)

References (20)
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  • 2
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    • An analysis of unsteady highly turbulent swirling flow in a model vortex combustor
    • Fernandez, E.C., Heitor, M.V., Shtork, S.I.: An Analysis of Unsteady Highly Turbulent Swirling Flow in a Model Vortex Combustor. Exp. Fluids, 40, pp. 177-187 (2006)
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  • 4
    • 10244222348 scopus 로고    scopus 로고
    • Unsteady flow structures in radial swirler fed fuel injectors
    • GT2004-53608
    • Midgley, K., Spencer, A., McGuirk, J.J.: Unsteady Flow Structures in Radial Swirler Fed Fuel Injectors. ASME Turbo Expo 2004, GT2004-53608
    • ASME Turbo Expo 2004
    • Midgley, K.1    Spencer, A.2    McGuirk, J.J.3
  • 5
    • 0002483755 scopus 로고
    • Time dependent boundary conditions for hyperbolic systems
    • Thompson, K.W.: Time Dependent Boundary Conditions for Hyperbolic Systems. J. of Comput. Phys., 68, pp. 1-24 (1987)
    • (1987) J. of Comput. Phys. , vol.68 , pp. 1-24
    • Thompson, K.W.1
  • 6
    • 0000009391 scopus 로고
    • Boundary conditions for direct simulations of compressible viscous flows
    • Poinsot, T., Lele, S.: Boundary Conditions for Direct Simulations of Compressible Viscous Flows. J. of Comput. Phys., 101, pp. 104-129 (1992)
    • (1992) J. of Comput. Phys. , vol.101 , pp. 104-129
    • Poinsot, T.1    Lele, S.2
  • 7
    • 33750841500 scopus 로고    scopus 로고
    • Accurate boundary conditions for the numerical simulation of thermoacoustic phenomena in gas-turbine combustion chambers
    • GT2006-90441
    • Widenhorn, A., Noll, B., Aigner, M.: Accurate Boundary Conditions for the Numerical Simulation of Thermoacoustic Phenomena in Gas-Turbine Combustion Chambers. ASME Turbo Expo 2006, GT2006-90441
    • ASME Turbo Expo 2006
    • Widenhorn, A.1    Noll, B.2    Aigner, M.3
  • 9
    • 84905739509 scopus 로고    scopus 로고
    • Numerical simulation of high frequency flow instabilities near an airblast atomizer
    • GT2001-0041
    • Noll, B., Schütz, H., Aigner, M.: Numerical Simulation of High Frequency Flow Instabilities Near an Airblast Atomizer. ASME Turbo Expo 2001, GT2001-0041
    • ASME Turbo Expo 2001
    • Noll, B.1    Schütz, H.2    Aigner, M.3
  • 12
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    • Two equation eddy viscosity turbulence models for engineering applications
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    • Spalart, P.R.1
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    • Detached eddy simulation of massively separated flows
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    • Periodic combustion instabilities in a swirl burner studied by phase-locked planar laser-induced fluorescence
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.