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The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness and Aerodynamic Loss with Film Cooling Hole Shape
journal contribution
posted on 2023-05-16, 12:48 authored by Jane SargisonJane Sargison, Guo, SM, Oldfield, MLG, Rawlinson, AJNo description available
History
Publication title
Heat Transfer in Gas Turbine Systems, Annals of The New York Academy of SciencesVolume
934Pagination
361-368ISSN
0077-8923Department/School
School of EngineeringPublisher
The New York Academy of SciencesPlace of publication
USARepository Status
- Restricted
