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Volumn 6, Issue PART C, 2008, Pages 2631-2640

Improving the turbine cooling conceptual design process

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS MODELS; COMPUTER MODELS; CONVENTIONAL DESIGN; COOLANT FLOW; DESIGN SPACES; PROTOTYPE MODELS; SYSTEM REPRESENTATION; TURBINE BLADE COOLING; TURBINE COOLING;

EID: 69949172504     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-51285     Document Type: Conference Paper
Times cited : (5)

References (21)
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  • 6
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    • Air Cooling of Turbine Blades and Vanes
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  • 7
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    • A New Method to Calculate the Coolant Requirements of a High-Temperature Gas Turbine Blade
    • Torbidoni, L., Horlock, J.H., 2005, "A New Method to Calculate the Coolant Requirements of a High-Temperature Gas Turbine Blade", Journal of Turbomachinary, Vol. 127 (1), pp. 191-199.
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    • Torbidoni, L.1    Horlock, J.H.2
  • 8
    • 0004133369 scopus 로고
    • Prentice Hall, Englewood Cliffs, NJ, USA
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    • (1962) Introduction to Design
    • Asimow, M.1
  • 11
    • 0034235099 scopus 로고    scopus 로고
    • Liquid Crystal Measurements of Heat Transfer and Surface Shear Stress
    • Ireland,P.T.,Jones,T.V.,2000,"Liquid Crystal Measurements of Heat Transfer and Surface Shear Stress", Meas. Sci. Technol. Vol. 11, pp. 969-986.
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    • Ireland, P.T.1    Jones, T.V.2
  • 12
    • 3242711520 scopus 로고    scopus 로고
    • Verdicchio, J.V., Dixon, J.A., Benito, D., Karl, A., Tham, K.M., 2004, Recent Developments in Gas Turbine Component Temperature Prediction Methods, Proceedings of the Institute of Mechanical Engineers Part A - Journal of Power and Energy, 218 (A4), pp. 241-255.
    • Verdicchio, J.V., Dixon, J.A., Benito, D., Karl, A., Tham, K.M., 2004, "Recent Developments in Gas Turbine Component Temperature Prediction Methods", Proceedings of the Institute of Mechanical Engineers Part A - Journal of Power and Energy, Vol.218 (A4), pp. 241-255.
  • 13
    • 34548708211 scopus 로고    scopus 로고
    • Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades
    • GT2003-38180, TurboExpo, June 6-9, Reno, USA
    • Dennis, B.H., Egorov, I.N., Sobieczky, H., Dulikravich, GS., Yoshmura, S., 2003, "Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades", Proceedings of the ASME turbo-expo 2003, GT2003-38180, TurboExpo, June 6-9, Reno, USA.
    • (2003) Proceedings of the ASME turbo-expo , pp. 2003
    • Dennis, B.H.1    Egorov, I.N.2    Sobieczky, H.3    Dulikravich, G.S.4    Yoshmura, S.5
  • 14
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    • Simultaneous Prediction of External Flow Field and Temperature in Internally Cooled 3-D Turbine Blade Material
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    • (2001) International Journal of Turbo and Jet Engines , vol.18 , pp. 47-58
    • Han, Z.K.1    Dennis, B.H.2    Dulikravich, G.S.3
  • 16
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    • The Development and Validation of Simple Empirical Models of Impingement Cooling from Full Surface Heat Transfer Coefficient Distributions
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    • Gillespie, D.R.H., Son, CM., Ireland, P.T., Dailey, GM., 2003, "The Development and Validation of Simple Empirical Models of Impingement Cooling from Full Surface Heat Transfer Coefficient Distributions", Proceedings of the ASME turbo-expo, GT 2005-68504, TurboExpo, June 6-9, Reno, USA.
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  • 17
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  • 21
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    • Chanteloup, D.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.