Numerical Simulation of Turbine Blade Heat Transfer Using Two-Equation Turbulence Models
The development of high performance gas turbines requires high turbine inlet temperatures that can lead to severe thermal stresses in the turbine blades, particularly in the first stages of the turbine. Therefore, the major objective of gasturbine designers is to determine the thermal and aero-dynam...
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| Format: | Thesis |
| Language: | English English |
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2000
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| Online Access: | http://psasir.upm.edu.my/id/eprint/10493/1/FK_2000_27.pdf |