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Effect of Endwall Contouring on a Transonic Turbine Blade Passage: Heat Transfer Performance
Effect of Endwall Contouring on a Transonic Turbine Blade Passage: Heat Transfer Performance
2016
Kapil Panchal
Santosh Abraham
Arnab Roy
Srinath V. Ekkad
Wing F. Ng
Andrew S. Lohaus
Michael E. Crawford
Keywords:
Control theory
Physics
Turbine blade
Heat transfer coefficient
Transonic
Computational fluid dynamics
Mach number
Contouring
Aerospace engineering
Heat transfer
Mechanical engineering
engineering simulation
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