Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring

Amy Mensch, Karen A. Thole

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Endwall contouring is a technique used to reduce the strength and development of three-dimensional secondary flows in a turbine vane or blade passage in a gas turbine. The secondary flows locally affect the external heat transfer, particularly on the endwall surface. The combination of external and internal convective heat transfer along with solid conduction determines component temperatures, which affect the service life of turbine components. A conjugate heat transfer model is used to measure the non-dimensional external surface temperature, known as overall effectiveness, of an endwall with non-Axisymmetric contouring. The endwall cooling methods include internal impingement cooling and external film cooling. Measured values of overall effectiveness show that endwall contouring reduces the impingement effectiveness alone, but increases the effectiveness of film cooling alone. Given the combined case of both impingement and film cooling, the laterally averaged overall effectiveness is not significantly changed between the flat and contoured endwall. Flowfield measurements indicate that the size and location of the passage vortex changes as film cooling is added and as the blowing ratio increases. Because endwall contouring can produce local effects on internal cooling and film cooling performance, the implications for heat transfer should be considered in endwall contour designs.

Original languageEnglish (US)
Title of host publicationHeat Transfer
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791856710, 9780791856710
DOIs
StatePublished - Jan 1 2015
EventASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada
Duration: Jun 15 2015Jun 19 2015

Publication series

NameProceedings of the ASME Turbo Expo
Volume5A

Other

OtherASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
CountryCanada
CityMontreal
Period6/15/156/19/15

Fingerprint

Cooling
Heat transfer
Secondary flow
Turbine components
Blow molding
Service life
Turbomachine blades
Gas turbines
Vortex flow
Turbines
Temperature

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Mensch, A., & Thole, K. A. (2015). Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring. In Heat Transfer (Proceedings of the ASME Turbo Expo; Vol. 5A). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2015-42706
Mensch, Amy ; Thole, Karen A. / Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring. Heat Transfer. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo).
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Mensch, A & Thole, KA 2015, Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring. in Heat Transfer. Proceedings of the ASME Turbo Expo, vol. 5A, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015, Montreal, Canada, 6/15/15. https://doi.org/10.1115/GT2015-42706

Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring. / Mensch, Amy; Thole, Karen A.

Heat Transfer. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo; Vol. 5A).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Mensch A, Thole KA. Overall effectiveness and flowfield measurements for an endwall with Non-Axisymmetric contouring. In Heat Transfer. American Society of Mechanical Engineers (ASME). 2015. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT2015-42706