메뉴 건너뛰기




Volumn 53, Issue 3, 2008, Pages 308-322

Computational investigation of film cooling from trenched holes near the leading edge of a turbine blade

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; COMPUTER SIMULATION; COOLING; FINITE VOLUME METHOD; NAVIER STOKES EQUATIONS; TURBINES; TURBOMACHINE BLADES;

EID: 36048989624     PISSN: 10407782     EISSN: 15210634     Source Type: Journal    
DOI: 10.1080/10407780701564200     Document Type: Article
Times cited : (34)

References (20)
  • 1
    • 0009736725 scopus 로고    scopus 로고
    • Heat Transfer on a Film-Cooled Rotating Blade
    • NASA/CR1999-209301, NASA Glenn Research Center, Cleveland, OH
    • V. K. Garg, Heat Transfer on a Film-Cooled Rotating Blade, NASA Rep. NASA/CR1999-209301, NASA Glenn Research Center, Cleveland, OH, 1999.
    • (1999) NASA Rep
    • Garg, V.K.1
  • 2
    • 0001347860 scopus 로고    scopus 로고
    • Film Cooling Predictions of Simple and Compound Angle Injection from One and Two Staggered Rows
    • A. Azzi, M. Abidat, B. A. Jubran, and G. S. Theodoridis, Film Cooling Predictions of Simple and Compound Angle Injection from One and Two Staggered Rows, Numer. Heat Transfer A, vol. 40, pp. 273-294, 2001.
    • (2001) Numer. Heat Transfer A , vol.40 , pp. 273-294
    • Azzi, A.1    Abidat, M.2    Jubran, B.A.3    Theodoridis, G.S.4
  • 3
    • 0029375536 scopus 로고
    • Comparison of Different Turbulence Models for Prediction of Slot-Film Cooling: Flow and Temperature Field
    • S. Sarkar and T. K. Bose, Comparison of Different Turbulence Models for Prediction of Slot-Film Cooling: Flow and Temperature Field, Numer. Heat Transfer B, vol. 28, pp. 217-238, 1995.
    • (1995) Numer. Heat Transfer B , vol.28 , pp. 217-238
    • Sarkar, S.1    Bose, T.K.2
  • 4
    • 84973651854 scopus 로고    scopus 로고
    • Investigation of Various Parametric Influences on Leading Edge Film Cooling
    • Orlando, FL, ASME Paper 97-GT-296
    • M. W. Cruse, U. M. Yuki, and D. Bogard, Investigation of Various Parametric Influences on Leading Edge Film Cooling, in Int. Gas Turbine & Aero Engine Congress & Exhibition, Orlando, FL, 1997, ASME Paper 97-GT-296.
    • (1997) Int. Gas Turbine & Aero Engine Congress & Exhibition
    • Cruse, M.W.1    Yuki, U.M.2    Bogard, D.3
  • 5
    • 0028195272 scopus 로고
    • An Experimental Study of Film Cooling Effectiveness near the Leading Edge of a Turbine Blade
    • M. Salcudean, I. Gartshore, K. Zhang, and I. McLean, An Experimental Study of Film Cooling Effectiveness near the Leading Edge of a Turbine Blade, J. Turbomachinery, vol. 116, pp. 71-79, 1994.
    • (1994) J. Turbomachinery , vol.116 , pp. 71-79
    • Salcudean, M.1    Gartshore, I.2    Zhang, K.3    McLean, I.4
  • 6
    • 0030576484 scopus 로고    scopus 로고
    • Leading Edge Film Cooling on Turbine Blade Heat Transfer
    • V. K. Garg and R. E. Gaugler, Leading Edge Film Cooling on Turbine Blade Heat Transfer, Numer. Heat Transfer A, vol. 30, pp. 165-187, 1996.
    • (1996) Numer. Heat Transfer A , vol.30 , pp. 165-187
    • Garg, V.K.1    Gaugler, R.E.2
  • 7
    • 21044455345 scopus 로고    scopus 로고
    • Influence of Leading-Edge Lateral Injection Angles on the Film Cooling Effectiveness of a Gas Turbine Blade
    • A. Azzi and B. A. Jubran, Influence of Leading-Edge Lateral Injection Angles on the Film Cooling Effectiveness of a Gas Turbine Blade, Heat Mass Transfer, vol. 40, pp. 501-508, 2004.
    • (2004) Heat Mass Transfer , vol.40 , pp. 501-508
    • Azzi, A.1    Jubran, B.A.2
  • 8
    • 36049042790 scopus 로고    scopus 로고
    • W. Haslinger and D. K. Hennecke, Highly Resolved Distribution of Adiabatic Film Cooling Effectiveness for Turbine Leading Edge Film Cooling, in Proc. 13th Int. Symp. Air Breathing Engines, Chattanooga, TN, ISBE 97-7113, American Institute of Aeronautics and Astronautics, 1997.
    • W. Haslinger and D. K. Hennecke, Highly Resolved Distribution of Adiabatic Film Cooling Effectiveness for Turbine Leading Edge Film Cooling, in Proc. 13th Int. Symp. Air Breathing Engines, Chattanooga, TN, ISBE 97-7113, American Institute of Aeronautics and Astronautics, 1997.
  • 9
    • 0035310925 scopus 로고    scopus 로고
    • Three-Dimensional Flow and Heat Transfer Calculations of Film Cooling at the Leading Edge of a Symmetrical Turbine Blade Model
    • D. Lakehal, G. S. Theodoridis, and W. Rodi, Three-Dimensional Flow and Heat Transfer Calculations of Film Cooling at the Leading Edge of a Symmetrical Turbine Blade Model, Int. J. Heat Fluid Flow, vol. 22, pp. 113-122, 2001.
    • (2001) Int. J. Heat Fluid Flow , vol.22 , pp. 113-122
    • Lakehal, D.1    Theodoridis, G.S.2    Rodi, W.3
  • 10
    • 0142156231 scopus 로고    scopus 로고
    • Influence of Shaped Injection Holes on Turbine Blade Leading Edge Film Cooling
    • Y. J. Kim and S. M. Kim, Influence of Shaped Injection Holes on Turbine Blade Leading Edge Film Cooling, Int. J. Heat Mass Transfer, vol. 47, pp. 245-256, 2004.
    • (2004) Int. J. Heat Mass Transfer , vol.47 , pp. 245-256
    • Kim, Y.J.1    Kim, S.M.2
  • 11
    • 33144478777 scopus 로고    scopus 로고
    • Experimental Investigations on Showerhead Cooling on a Blunt Body
    • C. Falcoz, B. Weigand, and P. Ott, Experimental Investigations on Showerhead Cooling on a Blunt Body, Int. J. Heat Mass Transfer, vol. 49, pp. 1287-1298, 2006.
    • (2006) Int. J. Heat Mass Transfer , vol.49 , pp. 1287-1298
    • Falcoz, C.1    Weigand, B.2    Ott, P.3
  • 12
    • 36049000718 scopus 로고    scopus 로고
    • Effect of Film-Hole Shape on Turbine Blade Film Cooling Performance
    • NASA/CR-2000-209932, Glenn Research Center, Cleveland, OH
    • J. C. Han and S. Teng, Effect of Film-Hole Shape on Turbine Blade Film Cooling Performance, NASA Rep. NASA/CR-2000-209932, Glenn Research Center, Cleveland, OH, 2000.
    • (2000) NASA Rep
    • Han, J.C.1    Teng, S.2
  • 13
    • 36048980753 scopus 로고    scopus 로고
    • Method for Improving the Cooling Effectiveness of a Gaseous Coolant Stream, and Related Articles of Manufacture,
    • U.S. Patent 6,234,755 B1, 2001
    • R. S. Bunker, J. C. Bailey, C. P. Lee, and N. Abuaf, Method for Improving the Cooling Effectiveness of a Gaseous Coolant Stream, and Related Articles of Manufacture, U.S. Patent 6,234,755 B1, 2001.
    • Bunker, R.S.1    Bailey, J.C.2    Lee, C.P.3    Abuaf, N.4
  • 16
    • 33845532553 scopus 로고    scopus 로고
    • Predictions of Film Cooling from Cylindrical Holes Embedded in Trenches
    • San Francisco, CA, AIAA Paper 2006-3401
    • Y. Lu and S. V. Ekkad, Predictions of Film Cooling from Cylindrical Holes Embedded in Trenches, 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conf, San Francisco, CA, 2006, AIAA Paper 2006-3401.
    • (2006) 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conf
    • Lu, Y.1    Ekkad, S.V.2
  • 17
    • 0026970868 scopus 로고
    • Three-Dimensional Finite-Volume Method for Incompressible Flows with Complex Boundaries
    • S. Majumdar, W. Rodi, and J. Zhu, Three-Dimensional Finite-Volume Method for Incompressible Flows with Complex Boundaries, J. Fluids Eng., vol. 114, pp. 496-503, 1992.
    • (1992) J. Fluids Eng , vol.114 , pp. 496-503
    • Majumdar, S.1    Rodi, W.2    Zhu, J.3
  • 18
    • 33845658750 scopus 로고    scopus 로고
    • An Improved Numerical Scheme for the SIMPLER Method on Nonorthogonal Curvilinear Coordinates: SIMPLERM
    • Z. G. Qu, Q. Q. Tao, and Y. L. He, An Improved Numerical Scheme for the SIMPLER Method on Nonorthogonal Curvilinear Coordinates: SIMPLERM, Numer. Heat Transfer, vol. 51, pp. 43-66, 2007.
    • (2007) Numer. Heat Transfer , vol.51 , pp. 43-66
    • Qu, Z.G.1    Tao, Q.Q.2    He, Y.L.3
  • 19
    • 4243193913 scopus 로고    scopus 로고
    • Film Cooling with Compound Angle Holes: Adiabatic Effectiveness
    • D. L. Schmidt, B. Sen, and D. G. Bogard, Film Cooling with Compound Angle Holes: Adiabatic Effectiveness, J. Turbomachinery, vol. 118, pp. 807-813, 1996.
    • (1996) J. Turbomachinery , vol.118 , pp. 807-813
    • Schmidt, D.L.1    Sen, B.2    Bogard, D.G.3
  • 20
    • 0026835009 scopus 로고
    • Comparison of Different Two-Equation Turbulence Models for Prediction of Film Cooling from Two Rows of Holes
    • A. Amer, B. A. Jubran, and M. A. Hamdan, Comparison of Different Two-Equation Turbulence Models for Prediction of Film Cooling from Two Rows of Holes, Numer. Heat Transfer A, vol. 21, pp. 143-162, 1992.
    • (1992) Numer. Heat Transfer A , vol.21 , pp. 143-162
    • Amer, A.1    Jubran, B.A.2    Hamdan, M.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.