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The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness and Aerodynamic Loss with Film Cooling Hole Shape

Citation

Sargison, JE and Guo, SM and Oldfield, MLG and Rawlinson, AJ, The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness and Aerodynamic Loss with Film Cooling Hole Shape, Heat Transfer in Gas Turbine Systems, Annals of The New York Academy of Sciences , 934 pp. 361-368. ISSN 0077-8923 (2001) [Refereed Article]

Item Details

Item Type:Refereed Article
Research Division:Engineering
Research Group:Aerospace Engineering
Research Field:Aerodynamics (excl. Hypersonic Aerodynamics)
Objective Division:Manufacturing
Objective Group:Transport Equipment
Objective Field:Aerospace Equipment
Author:Sargison, JE (Dr Jane Sargison)
ID Code:21509
Year Published:2001
Web of Science® Times Cited:5
Deposited By:Engineering
Deposited On:2002-01-03
Last Modified:2011-10-07
Downloads:0

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