This paper presents detailed phase-resolved heat-flux data obtained on rotor blades and a comparison of simultaneously obtained time-resolved heat-flux and static pressure data obtained on the stationary shroud of a Garrett TFE 731-2 HP full-stage rotating turbine. A shock tube is used to generate a short-duration source of heated and pressurized air and platinum thin-film gages are used to obtain heat-flux measurements. Blade results are presented at several selected blade locations. Shroud surface pressure and heat-flux time histories are presented for comparable locations relative to the blade position. For these measurements, the turbine was operating at the design flow function, the design stage pressure ratio, and at 100% corrected speed.
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ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
June 4–8, 1989
Toronto, Ontario, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7916-0
PROCEEDINGS PAPER
Phase and Time-Resolved Measurements of Unsteady Heat Transfer and Pressure in a Full-Stage Rotating Turbine
M. G. Dunn
M. G. Dunn
Calspan-UB Research Center, Buffalo, NY
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M. G. Dunn
Calspan-UB Research Center, Buffalo, NY
Paper No:
89-GT-135, V004T08A014; 9 pages
Published Online:
March 18, 2015
Citation
Dunn, MG. "Phase and Time-Resolved Measurements of Unsteady Heat Transfer and Pressure in a Full-Stage Rotating Turbine." Proceedings of the ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition. Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration. Toronto, Ontario, Canada. June 4–8, 1989. V004T08A014. ASME. https://doi.org/10.1115/89-GT-135
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