Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing

Hamidur Md. Rahman, Sung In Kim, Ibrahim Hassan, Carole El Ayoubi

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

7 Citations (Scopus)

Abstract

An unsteady numerical investigation was performed to examine time dependent behaviors of the tip leakage flow structures and heat transfer on the rotor blade tip and casing in a single stage gas turbine engine. A transonic, high-pressure turbine stage was modeled and simulated using a stage pressure ratio of 3.2. The rotor's tip clearance was 1.2 mm in height (3% of the rotor span) and its speed was set at 9500 rpm. Periodic flow is observed for each vane passing period. Tip leakage flow as well as heat transfer data showed highly time dependent behaviors. A stator trailing edge shock appears as the turbine stage is operating at transonic conditions. The shock alters the flow condition in the rotor section, namely, the tip leakage flow structures and heat transfer rate distributions. The instantaneous Nusselt number distributions are compared to the time averaged and steady-state results. The same patterns in tip leakage flow structures and heat transfer rate distributions were observed in both unsteady and steady simulations. However, the unsteady simulation captured the locally time-dependent high heat transfer phenomena caused by the unsteady interaction with the upstream vane trailing-edge shock and the passing wake.

Original languageEnglish
Title of host publicationASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
Pages2353-2362
Number of pages10
Volume7
EditionPARTS A, B, AND C
DOIs
Publication statusPublished - 2010
Externally publishedYes
EventASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 - Glasgow, United Kingdom
Duration: 14 Jun 201018 Jun 2010

Other

OtherASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
CountryUnited Kingdom
CityGlasgow
Period14/6/1018/6/10

Fingerprint

Turbomachine blades
Turbines
Heat transfer
Flow structure
Rotors
Nusselt number
Stators
Gas turbines

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Md. Rahman, H., Kim, S. I., Hassan, I., & El Ayoubi, C. (2010). Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing. In ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 (PARTS A, B, AND C ed., Vol. 7, pp. 2353-2362) https://doi.org/10.1115/GT2010-22104

Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing. / Md. Rahman, Hamidur; Kim, Sung In; Hassan, Ibrahim; El Ayoubi, Carole.

ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. Vol. 7 PARTS A, B, AND C. ed. 2010. p. 2353-2362.

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

Md. Rahman, H, Kim, SI, Hassan, I & El Ayoubi, C 2010, Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing. in ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A, B, AND C edn, vol. 7, pp. 2353-2362, ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010, Glasgow, United Kingdom, 14/6/10. https://doi.org/10.1115/GT2010-22104
Md. Rahman H, Kim SI, Hassan I, El Ayoubi C. Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing. In ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. PARTS A, B, AND C ed. Vol. 7. 2010. p. 2353-2362 https://doi.org/10.1115/GT2010-22104
Md. Rahman, Hamidur ; Kim, Sung In ; Hassan, Ibrahim ; El Ayoubi, Carole. / Unsteady tip leakage flow characteristics and heat transfer on turbine blade tip and casing. ASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010. Vol. 7 PARTS A, B, AND C. ed. 2010. pp. 2353-2362
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