A research and development program has been undertaken to ascertain the effects of surface roughness levels on vane external heat transfer, with varied conditions of inlet freestream turbulence intensity and vane Reynolds number. A transonic linear vane cascade was constructed to operate at a nominal overall pressure ratio of 1.86. Airfoil heat transfer distributions are measured using a thin-walled stainless steel airfoil having imbedded thermocouples. The methodology incorporates a thin-foil surface heater to provide a known heat flux condition, with room temperature mainstream air at approximately 5 atm pressure. Heat transfer is characterized for uniform surface average roughness levels of 0.4, 1.85, and 4.5 micrometers, with inlet turbulence intensity levels from 4 to 13%. Airfoil Reynolds number based on axial chord length and exit velocity ranges from 2.2 to 4.8 · 106. Results show consistent individual and combined effects of Reynolds number, turbulence, and surface roughness changes. Higher roughness levels tend to dominate turbulence effects in most regions except the leading edge.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7870-5
PROCEEDINGS PAPER
Separate and Combined Effects of Surface Roughness and Turbulence Intensity on Vane Heat Transfer
Ronald S. Bunker
Ronald S. Bunker
General Electric Company, Schenectady, NY
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Ronald S. Bunker
General Electric Company, Schenectady, NY
Paper No:
97-GT-135, V003T09A022; 10 pages
Published Online:
December 24, 2014
Citation
Bunker, RS. "Separate and Combined Effects of Surface Roughness and Turbulence Intensity on Vane Heat Transfer." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration. Orlando, Florida, USA. June 2–5, 1997. V003T09A022. ASME. https://doi.org/10.1115/97-GT-135
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