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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 |
| UTAS Author: | Sargison, JE (Dr Jane Sargison) |
| ID Code: | 21509 |
| Year Published: | 2001 |
| Web of Science® Times Cited: | 6 |
| Deposited By: | Engineering |
| Deposited On: | 2002-01-03 |
| Last Modified: | 2011-10-07 |
| Downloads: | 0 |
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