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The effects of turbulence and stator/rotor interactions on turbine heat transfer. II - Effects of Reynolds number and incidencePart I of this paper presents airfoil heat transfer data obtained in a rotating turbine model at its design rotor incidence. This portion of the paper presents heat transfer data obtained in the same model for various combinations of Reynolds number and inlet turbulence and for a very wide range of rotor incidence. On the suction surfaces of the first stage airfoils the locations and lengths of transition were influenced by both the inlet turbulence level and the Reynolds number. In addition it was demonstrated that on the first stage pressure surfaces combinations of high Reynolds number and high turbulence can produce heat transfer rates well in excess of two-dimensional turbulent flow. Rotor heat transfer distributions indicate that for relatively small deviations from the design incidence, local changes to the heat transfer distributions were produced on both pressure and suction sides near the stagnation region. For extremely large negative incidence the flow was completely separated from the rotor pressure surface producing very high local heat transfer.
Document ID
19880066925
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blair, M. F.
(United Technologies Research Center East Hartford, CT, United States)
Dring, R. P.
(United Technologies Research Center East Hartford, CT, United States)
Joslyn, H. D.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ASME PAPER 88-GT-5
Accession Number
88A54152
Funding Number(s)
CONTRACT_GRANT: NAS3-23717
Distribution Limits
Public
Copyright
Other

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