Local Mass and Heat Transfer on a Turbine Blade Tip

Local mass and heat transfer measurements on a simulated high-pressure turbine blade-tip surface are conducted in a linear cascade with a nonmoving tip endwall, using a naphthalene sublimation technique. The effects of tip clearance (0.86–6.90% of chord) are investigated at various exit Reynolds num...

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Bibliographic Details
Main Authors: P. Jin, R. J. Goldstein
Format: Article
Published: Hindawi Limited 2003-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/S1023621X03000083