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Volumn 8, Issue 3, 2000, Pages 283-308

Multidisciplinary optimization for gas turbine airfoil design

Author keywords

Cooled turbine; Film cooling; Heat transfer; Multiobjective optimization

Indexed keywords


EID: 0001250312     PISSN: 10682767     EISSN: None     Source Type: Journal    
DOI: 10.1080/174159700088027731     Document Type: Article
Times cited : (10)

References (29)
  • 2
    • 0015200014 scopus 로고
    • Film Cooling
    • Academic Press, New York and London
    • Goldstein, R. J. (1971). Film Cooling, Advances in Heat Transfer, Academic Press, New York and London, 7, 321-379.
    • (1971) Advances in Heat Transfer , vol.7 , pp. 321-379
    • Goldstein, R.J.1
  • 3
    • 84923902230 scopus 로고    scopus 로고
    • Navier-Stokes Simulation of the Flow Around a Leading Edge Film-Cooled Turbine Blade Including the Interior Cooling System and Comparison with Experimental Data
    • UK, June 10-13, Paper No. 96-GT-71
    • Vogel, D. T., Navier-Stokes Simulation of the Flow Around a Leading Edge Film-Cooled Turbine Blade Including the Interior Cooling System and Comparison with Experimental Data, Proceedings of the International Gas. Turbine and Aeroengine Congress and Exhibition, Birmingham, UK, June 10-13, 1996, Paper No. 96-GT-71.
    • (1996) Proceedings of the International Gas. Turbine and Aeroengine Congress and Exhibition, Birmingham
    • Vogel, D.T.1
  • 4
    • 0021313707 scopus 로고
    • Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades
    • Tokyo, Japan, October 24-28, Paper No. ASME 95-GT-2
    • Eckert, E. R. G., Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades, Proceedings of the Tokyo International Gas Turbine Congress, Tokyo, Japan, October 24-28, 1983, Paper No. ASME 95-GT-2.
    • (1983) Proceedings of the Tokyo International Gas Turbine Congress
    • Eckert, E.R.G.1
  • 5
    • 0021936782 scopus 로고
    • Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces
    • January
    • Hay, N., Lampard, D. and Saluja, C. L., Effects of the Condition of the Approach Boundary Layer and of Mainstream Pressure Gradients on the Heat Transfer Coefficient on Film-Cooled Surfaces, Journal of Engineering for Gas Turbines and Power, 107, January, 1985, 99-104.
    • (1985) Journal of Engineering for Gas Turbines and Power , vol.107 , pp. 99-104
    • Hay, N.1    Lampard, D.2    Saluja, C.L.3
  • 7
    • 0026938730 scopus 로고
    • Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Spacing
    • Mehendale, B. and Han, J. C. (1992). Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Spacing, International Journal of Heat and Mass Transfer, 35(10), 2593-2604.
    • (1992) International Journal of Heat and Mass Transfer , vol.35 , Issue.10 , pp. 2593-2604
    • Mehendale, B.1    Han, J.C.2
  • 8
    • 0031441576 scopus 로고    scopus 로고
    • A Systematic Computational Methodology Applied to a Three-Dimensional Film-Cooling Flowfield
    • October
    • Walters, D. K. and Leylek, J. H., A Systematic Computational Methodology Applied to a Three-Dimensional Film-Cooling Flowfield, Journal of Turbomachinery, 119, October, 1997, 777-785.
    • (1997) Journal of Turbomachinery , vol.119 , pp. 777-785
    • Walters, D.K.1    Leylek, J.H.2
  • 10
    • 84983177854 scopus 로고
    • Three-Dimensional Coolant Passage Design for Specified Temperature and Heat Fluxes
    • AIAA Paper No. 94-0348, Reno, Nevada
    • Dulikravich, G. S. and Martin, T. J., Three-Dimensional Coolant Passage Design for Specified Temperature and Heat Fluxes, AIAA Paper No. 94-0348, 32nd Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 1994.
    • (1994) 32nd Aerospace Sciences Meeting and Exhibit
    • Dulikravich, G.S.1    Martin, T.J.2
  • 11
    • 0006993506 scopus 로고    scopus 로고
    • Braembussche, Three-Dimensional Inverse Method for Turbomachinery Blade Design
    • April
    • Demeulenaere, A. and Van den R., Braembussche, Three-Dimensional Inverse Method for Turbomachinery Blade Design, Journal of Turbomachinery, 120, April, 1998, 247-255.
    • (1998) Journal of Turbomachinery , vol.120 , pp. 247-255
    • Demeulenaere, A.1    Van Den, R.2
  • 12
    • 0026944950 scopus 로고
    • Aerodynamic Shape Design and Optimization: Status and Trends
    • Nov.-Dec.
    • Dulikravich, G. S., Aerodynamic Shape Design and Optimization: Status and Trends, Journal of Aircraft, 29(6), Nov.-Dec., 1992, 1020-1026.
    • (1992) Journal of Aircraft , vol.29 , Issue.6 , pp. 1020-1026
    • Dulikravich, G.S.1
  • 17
    • 84978773116 scopus 로고    scopus 로고
    • Dennis, Minimization of Coolant Mass Flow Rate in Internally Cooled Gas Turbine Blades
    • Paper No. ASME 99-GT-146, June 7-10, Indianapolis, Indiana
    • Martin, T. J., Dulikravich, G. S., Shen-Xue, Han and Brian H., Dennis, Minimization of Coolant Mass Flow Rate in Internally Cooled Gas Turbine Blades, International Gas Turbine and Aeroengine Congress and Exhibition, Paper No. ASME 99-GT-146, June 7-10, 1999, Indianapolis, Indiana.
    • (1999) International Gas Turbine and Aeroengine Congress and Exhibition
    • Martin, T.J.1    Dulikravich, G.S.2    Han, S.-X.3    Brian, H.4
  • 19
    • 0023409961 scopus 로고
    • Explicit Multigrid Algorithm for Quasi-Three-Dimensional Viscous Flows in Turbomachinery
    • Chima, R. V. (1987). Explicit Multigrid Algorithm for Quasi-Three-Dimensional Viscous Flows in Turbomachinery, Journal of Propulsion, 3(5), 397-405.
    • (1987) Journal of Propulsion , vol.3 , Issue.5 , pp. 397-405
    • Chima, R.V.1
  • 26
    • 0029455578 scopus 로고
    • A Coupled Rotor/Wing Optimization Procedure of High Speed Tilt-Rotor Aircraft
    • May 9-11, Fort Worth, Texas
    • McCarthy, T., Chattopadhyay, A. and Zhang, S., A Coupled Rotor/Wing Optimization Procedure of High Speed Tilt-Rotor Aircraft, presented at the 51st Annual Forum of the AHS, May 9-11, 1995, Fort Worth, Texas.
    • (1995) 51st Annual Forum of the AHS
    • McCarthy, T.1    Chattopadhyay, A.2    Zhang, S.3
  • 27
    • 0030289622 scopus 로고    scopus 로고
    • Optimization Procedure with Analytical Aerodynamic Sensitivity for Reduced Sonic Boom Design
    • Pagaldipti, N. S., Narayan, J. R. and Chattopadhyay, A. (1996). Optimization Procedure With Analytical Aerodynamic Sensitivity for Reduced Sonic Boom Design, AIAA Journal of Aircraft, 33(6), 1123-1130.
    • (1996) AIAA Journal of Aircraft , vol.33 , Issue.6 , pp. 1123-1130
    • Pagaldipti, N.S.1    Narayan, J.R.2    Chattopadhyay, A.3
  • 29
    • 0000968422 scopus 로고
    • Two-Point Exponential Approximation Method for Structural Optimization
    • Fadel, G. M., Riley, M. F. and Barthelemy, J. F. M. (1990). Two-Point Exponential Approximation Method for Structural Optimization, Structural Optimization, 2, 117-124.
    • (1990) Structural Optimization , vol.2 , pp. 117-124
    • Fadel, G.M.1    Riley, M.F.2    Barthelemy, J.F.M.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.