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Volumn 26, Issue 3, 2005, Pages 349-361

Flow analyses in a high-pressure axial ventilation fan with a non-linear eddy-viscosity closure

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; HIGH PRESSURE EFFECTS; MATHEMATICAL MODELS; REYNOLDS NUMBER; TURBULENCE; VENTILATION; VISCOSITY;

EID: 16844376838     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijheatfluidflow.2004.10.002     Document Type: Article
Times cited : (61)

References (41)
  • 1
    • 0031291421 scopus 로고    scopus 로고
    • Prediction of Francis turbine runner performance using a 3D finite element technique with unassembled stiffness matrix treatment
    • 2nd European Conf. on Turbomachinery Antwerp, Belgium
    • Borello D. Corsini A. Rispoli F. 1997 Prediction of Francis turbine runner performance using a 3D finite element technique with unassembled stiffness matrix treatment. In: 2nd European Conf. on Turbomachinery, Antwerp, Belgium
    • (1997)
    • Borello, D.1    Corsini, A.2    Rispoli, F.3
  • 2
    • 10244234562 scopus 로고    scopus 로고
    • A multi-grid additive and distributive parallel algorithm for finite element turbomachinery CFD
    • ECCOMAS-CFD 2001, Swansea, UK
    • Borello D. Borrelli P. Quagliata E. Rispoli F. 2001 A multi-grid additive and distributive parallel algorithm for finite element turbomachinery CFD. ECCOMAS-CFD 2001, Swansea, UK
    • (2001)
    • Borello, D.1    Borrelli, P.2    Quagliata, E.3    Rispoli, F.4
  • 3
    • 0037411943 scopus 로고    scopus 로고
    • A finite element overlapping scheme for turbomachinery flows on parallel platforms
    • D. Borello A. Corsini F. Rispoli A finite element overlapping scheme for turbomachinery flows on parallel platforms Comput. Fluids 32 7 2003 1017-1047
    • (2003) Comput. Fluids , vol.32 , Issue.7 , pp. 1017-1047
    • Borello, D.1    Corsini, A.2    Rispoli, F.3
  • 4
    • 27744440481 scopus 로고    scopus 로고
    • Modeling turbomachine-blade flows with non-linear eddy-viscosity models and second moment closure
    • IMechE Paper C557/131/99, A
    • Chen W.L. Leschziner M.A. 1999 Modeling turbomachine-blade flows with non-linear eddy-viscosity models and second moment closure. IMechE Paper C557/131/99, A, pp. 189-199
    • (1999) , pp. 189-199
    • Chen, W.L.1    Leschziner, M.A.2
  • 5
    • 0032144306 scopus 로고    scopus 로고
    • Computational prediction of flow around highly loaded compressor - Cascade blades with non-linear eddy-viscosity models
    • W.L. Chen F.S. Lien M.A. Leschziner Computational prediction of flow around highly loaded compressor - cascade blades with non-linear eddy-viscosity models Int. J. Heat Fluid Flow 19 1998 307-319
    • (1998) Int. J. Heat Fluid Flow , vol.19 , pp. 307-319
    • Chen, W.L.1    Lien, F.S.2    Leschziner, M.A.3
  • 6
    • 0018935743 scopus 로고
    • On the calculation of turbulent heat transport downstream from an abrupt pipe expansion
    • C.C. Chieng B.E. Launder On the calculation of turbulent heat transport downstream from an abrupt pipe expansion Numer. Heat Transfer 3 1980 189-207
    • (1980) Numer. Heat Transfer , vol.3 , pp. 189-207
    • Chieng, C.C.1    Launder, B.E.2
  • 7
    • 0031921967 scopus 로고    scopus 로고
    • Calculation of tip clearance effects in a transonic compressor rotor
    • R.V. Chima Calculation of tip clearance effects in a transonic compressor rotor J. Turbomach. 120 1998 131-140
    • (1998) J. Turbomach. , vol.120 , pp. 131-140
    • Chima, R.V.1
  • 8
    • 0029673650 scopus 로고    scopus 로고
    • The effect of tip clearance on a swept transonic compressor rotor
    • W.W. Copenhaver E.R. Mayhew C. Hah A.R. Wadia The effect of tip clearance on a swept transonic compressor rotor J. Turbomach. 118 1996 230-239
    • (1996) J. Turbomach. , vol.118 , pp. 230-239
    • Copenhaver, W.W.1    Mayhew, E.R.2    Hah, C.3    Wadia, A.R.4
  • 9
    • 0013502062 scopus 로고    scopus 로고
    • Numerical simulation of three-dimensional viscous flow in an isolated axial rotor
    • XLVI-4
    • A. Corsini F. Rispoli Numerical simulation of three-dimensional viscous flow in an isolated axial rotor Arch. Mech. Eng. XLVI-4 1999 369-392
    • (1999) Arch. Mech. Eng. , pp. 369-392
    • Corsini, A.1    Rispoli, F.2
  • 10
    • 2542469208 scopus 로고    scopus 로고
    • Anisotropic turbulence modeling of near wall effects pertinent to turbomachinery flows
    • ASME Paper FEDSM02-31206
    • Corsini A. Rispoli F. 2002 Anisotropic turbulence modeling of near wall effects pertinent to turbomachinery flows. ASME Paper FEDSM02-31206
    • (2002)
    • Corsini, A.1    Rispoli, F.2
  • 11
    • 16844381284 scopus 로고    scopus 로고
    • The role of forward sweep in subsonic axial fan rotor aerodynamics at design and off-design operating conditions
    • ASME Paper GT2003-38671
    • Corsini A. Rispoli F. 2003 The role of forward sweep in subsonic axial fan rotor aerodynamics at design and off-design operating conditions. ASME Paper GT2003-38671
    • (2003)
    • Corsini, A.1    Rispoli, F.2
  • 12
    • 0001904657 scopus 로고    scopus 로고
    • Concerted experimental and numerical studies on axial flow fan rotor aerodynamics
    • IMechE Paper C557/106/99, B
    • Corsini A. Rispoli F. Bencze F. Vad J. 1999 Concerted experimental and numerical studies on axial flow fan rotor aerodynamics. IMechE Paper C557/106/99, B, pp. 519-531
    • (1999) , pp. 519-531
    • Corsini, A.1    Rispoli, F.2    Bencze, F.3    Vad, J.4
  • 13
    • 16844383596 scopus 로고    scopus 로고
    • Effects of blade sweep in a high performance axial flow rotor
    • ATI-CST Paper 005/01, 4th European Conf. on Turbomachinery, Firenze, Italy
    • Corsini A. Rispoli F. Bencze F. Vad J. 2001 Effects of blade sweep in a high performance axial flow rotor. ATI-CST Paper 005/01, 4th European Conf. on Turbomachinery, Firenze, Italy
    • (2001)
    • Corsini, A.1    Rispoli, F.2    Bencze, F.3    Vad, J.4
  • 14
    • 16844374741 scopus 로고    scopus 로고
    • A new stabilized finite element method for advection-diffusion-reaction equations using quadratic elements
    • T. Lajos et al. (Eds.) Springer-Verlag
    • A. Corsini F. Rispoli A. Santoriello A new stabilized finite element method for advection-diffusion-reaction equations using quadratic elements In: T. Lajos et al. (Eds.) Modelling Fluid Flow 2004 Springer-Verlag
    • (2004) Modelling Fluid Flow
    • Corsini, A.1    Rispoli, F.2    Santoriello, A.3
  • 15
    • 0030130491 scopus 로고    scopus 로고
    • Development and application of a cubic eddy-viscosity model of turbulence
    • T.J. Craft B.E. Launder K. Suga Development and application of a cubic eddy-viscosity model of turbulence Int. J. Heat Fluid Flow 17 1996 108-155
    • (1996) Int. J. Heat Fluid Flow , vol.17 , pp. 108-155
    • Craft, T.J.1    Launder, B.E.2    Suga, K.3
  • 16
    • 0030087363 scopus 로고    scopus 로고
    • On the k-ε stagnation point anomaly
    • P.A. Durbin On the k-ε stagnation point anomaly Int. J. Heat Fluid Flow 17 1996 89-90
    • (1996) Int. J. Heat Fluid Flow , vol.17 , pp. 89-90
    • Durbin, P.A.1
  • 18
    • 0032194368 scopus 로고    scopus 로고
    • Effects of stream surface inclination on tip leakage flow fields in compressor rotor
    • M. Furukawa K. Saiki K. Nagayoshi M. Kuroumaru M. Inoue Effects of stream surface inclination on tip leakage flow fields in compressor rotor J. Turbomach. 120 1998 683-694
    • (1998) J. Turbomach. , vol.120 , pp. 683-694
    • Furukawa, M.1    Saiki, K.2    Nagayoshi, K.3    Kuroumaru, M.4    Inoue, M.5
  • 19
    • 0032724551 scopus 로고    scopus 로고
    • The role of tip leakage vortex breakdown in compressor rotor aerodynamics
    • M. Furukawa M. Inoue K. Saiki K. Yamada The role of tip leakage vortex breakdown in compressor rotor aerodynamics J. Turbomach. 121 1999 469-480
    • (1999) J. Turbomach. , vol.121 , pp. 469-480
    • Furukawa, M.1    Inoue, M.2    Saiki, K.3    Yamada, K.4
  • 20
    • 0036820583 scopus 로고    scopus 로고
    • The use of sweep and dihedral in multistage axial flow compressor blading. Part II: Low and high-speed designs and test verification
    • S.J. Gallimore J.J. Bolger N.A. Cumpsty M.J. Taylor P.I. Wright J.M.M. Place The use of sweep and dihedral in multistage axial flow compressor blading. Part II: Low and high-speed designs and test verification J. Turbomach. 124 2002a 533-541
    • (2002) J. Turbomach. , vol.124 , pp. 533-541
    • Gallimore, S.J.1    Bolger, J.J.2    Cumpsty, N.A.3    Taylor, M.J.4    Wright, P.I.5    Place, J.M.M.6
  • 21
    • 0036821005 scopus 로고    scopus 로고
    • The use of sweep and dihedral in multistage axial flow compressor blading. Part I: University research and methods development
    • S.J. Gallimore J.J. Bolger N.A. Cumpsty M.J. Taylor P.I. Wright J.M.M. Place The use of sweep and dihedral in multistage axial flow compressor blading. Part I: University research and methods development J. Turbomach. 124 2002b 521-532
    • (2002) J. Turbomach. , vol.124 , pp. 521-532
    • Gallimore, S.J.1    Bolger, J.J.2    Cumpsty, N.A.3    Taylor, M.J.4    Wright, P.I.5    Place, J.M.M.6
  • 22
    • 0036186595 scopus 로고    scopus 로고
    • Improved prediction of turbomachinery flows using near-wall Reynolds-stress model
    • G.A. Gerolymos J. Neubauer V.C. Sharma I. Vallet Improved prediction of turbomachinery flows using near-wall Reynolds-stress model J. Turbomach. 121 2002 86-99
    • (2002) J. Turbomach. , vol.121 , pp. 86-99
    • Gerolymos, G.A.1    Neubauer, J.2    Sharma, V.C.3    Vallet, I.4
  • 23
    • 21144473351 scopus 로고
    • A comparison of the measured and predicted flow field in a modern by-pass configuration
    • R.K. Goyal W.N. Dawes A comparison of the measured and predicted flow field in a modern by-pass configuration J. Turbomach. 115 1993 273-282
    • (1993) J. Turbomach. , vol.115 , pp. 273-282
    • Goyal, R.K.1    Dawes, W.N.2
  • 24
    • 0022506373 scopus 로고
    • A numerical modeling of endwall and tip-clearance flow of an isolated compressor rotor
    • C. Hah A numerical modeling of endwall and tip-clearance flow of an isolated compressor rotor J. Eng. Power 108 1986 15-21
    • (1986) J. Eng. Power , vol.108 , pp. 15-21
    • Hah, C.1
  • 25
    • 0032979642 scopus 로고    scopus 로고
    • Development of hub corner stall and its influence on the performance of axial compressor blade rows
    • C. Hah J. Loellbach Development of hub corner stall and its influence on the performance of axial compressor blade rows J. Turbomach. 121 1999 67-77
    • (1999) J. Turbomach. , vol.121 , pp. 67-77
    • Hah, C.1    Loellbach, J.2
  • 26
    • 0026143135 scopus 로고
    • Three-dimensional flowfields inside a transonic compressor with swept blades
    • C. Hah A.J. Wennerstrom Three-dimensional flowfields inside a transonic compressor with swept blades J. Turbomach. 113 1991 241-251
    • (1991) J. Turbomach. , vol.113 , pp. 241-251
    • Hah, C.1    Wennerstrom, A.J.2
  • 27
    • 0030465082 scopus 로고    scopus 로고
    • Numerical simulation of three-dimensional viscous flow in a linear compressor cascade with tip clearance
    • S. Kang C. Hirsch Numerical simulation of three-dimensional viscous flow in a linear compressor cascade with tip clearance J. Turbomach. 118 1996 492-505
    • (1996) J. Turbomach. , vol.118 , pp. 492-505
    • Kang, S.1    Hirsch, C.2
  • 28
    • 49549151853 scopus 로고
    • Application to the energy-dissipation model of turbulence to the calculation of flow near a spinning disc
    • B.E. Launder B.I. Sharma Application to the energy-dissipation model of turbulence to the calculation of flow near a spinning disc Int. J. Heat Mass Transfer 1 1974 131-138
    • (1974) Int. J. Heat Mass Transfer , vol.1 , pp. 131-138
    • Launder, B.E.1    Sharma, B.I.2
  • 29
    • 4243152034 scopus 로고    scopus 로고
    • Flow analyses in a single-stage propulsion pump
    • Y.T. Lee C. Hah J. Loellbach Flow analyses in a single-stage propulsion pump J. Turbomach. 118 1996 240-249
    • (1996) J. Turbomach. , vol.118 , pp. 240-249
    • Lee, Y.T.1    Hah, C.2    Loellbach, J.3
  • 31
    • 0014763829 scopus 로고
    • Toward a turbulent constitutive relation
    • J.L. Lumley Toward a turbulent constitutive relation J. Fluid Mech. 41 1970 413-434
    • (1970) J. Fluid Mech. , vol.41 , pp. 413-434
    • Lumley, J.L.1
  • 32
    • 0036679877 scopus 로고    scopus 로고
    • Transition on a flat plate with a semi-circular leading edge under uniform and positive shear free-stream flow
    • A. Palikaras K. Yakinthos A. Goulas Transition on a flat plate with a semi-circular leading edge under uniform and positive shear free-stream flow Int. J. Heat Fluid Flow 23 2002 421-430
    • (2002) Int. J. Heat Fluid Flow , vol.23 , pp. 421-430
    • Palikaras, A.1    Yakinthos, K.2    Goulas, A.3
  • 33
    • 0016570251 scopus 로고
    • A more general effective-viscosity hypothesis
    • S.B. Pope A more general effective-viscosity hypothesis J. Fluid Mech. 72 1975 331-340
    • (1975) J. Fluid Mech. , vol.72 , pp. 331-340
    • Pope, S.B.1
  • 34
    • 2542494515 scopus 로고
    • Application of sweep to improve efficiency of a transonic fan: Part II. Performance and laser test results
    • AIAA paper 91-2544
    • Rabe D. Hoying D. Koff S. 1991 Application of sweep to improve efficiency of a transonic fan: Part II. Performance and laser test results, AIAA paper 91-2544
    • (1991)
    • Rabe, D.1    Hoying, D.2    Koff, S.3
  • 35
    • 0001008393 scopus 로고
    • The relation between the flow of non-Newtonian fluids and turbulent Newtonian fluids
    • R.S. Rivlin The relation between the flow of non-Newtonian fluids and turbulent Newtonian fluids Quart. Appl. Math. 15 1957 212-215
    • (1957) Quart. Appl. Math. , vol.15 , pp. 212-215
    • Rivlin, R.S.1
  • 36
    • 0026143134 scopus 로고
    • Tip leakage flow in axial compressors
    • J.A. Storer N.A. Cumpsty Tip leakage flow in axial compressors J. Turbomach. 113 1991 252-259
    • (1991) J. Turbomach. , vol.113 , pp. 252-259
    • Storer, J.A.1    Cumpsty, N.A.2
  • 37
    • 0032451585 scopus 로고    scopus 로고
    • Three-dimensional flow in axial flow fans of non-free vortex design
    • J. Vad F. Bencze Three-dimensional flow in axial flow fans of non-free vortex design Int. J. Heat Fluid Flow 19 1998 601-607
    • (1998) Int. J. Heat Fluid Flow , vol.19 , pp. 601-607
    • Vad, J.1    Bencze, F.2
  • 38
    • 0034541762 scopus 로고    scopus 로고
    • Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors
    • D.E. Van Zante A.J. Strazisar J.R. Wood M.D. Hathaway T.H. Okiishi Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors J. Turbomach. 122 2000 733-742
    • (2000) J. Turbomach. , vol.122 , pp. 733-742
    • Van Zante, D.E.1    Strazisar, A.J.2    Wood, J.R.3    Hathaway, M.D.4    Okiishi, T.H.5
  • 39
    • 0004070568 scopus 로고    scopus 로고
    • Inner working of aerodynamic sweep
    • ASME Paper 97-GT-401
    • Wadia A.R. Szucs P.N. Crall D.W. 1997 Inner working of aerodynamic sweep. ASME Paper 97-GT-401
    • (1997)
    • Wadia, A.R.1    Szucs, P.N.2    Crall, D.W.3
  • 40
    • 0021455795 scopus 로고
    • Experimental study of a high-through-flow transonic axial compressor stage
    • A.J. Wennerstrom Experimental study of a high-through-flow transonic axial compressor stage J. Gas Turbine Power 106 1984 552-560
    • (1984) J. Gas Turbine Power , vol.106 , pp. 552-560
    • Wennerstrom, A.J.1
  • 41
    • 0003767048 scopus 로고
    • The measurement of boundary layers on a compressor blade in cascade
    • NASA-CR-185118
    • Zierke W.C. Deutsch S. 1989 The measurement of boundary layers on a compressor blade in cascade, vol. 2. Data Tables and Final Report. NASA-CR-185118
    • (1989) Data Tables and Final Report , vol.2
    • Zierke, W.C.1    Deutsch, S.2


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