Investigation on the differences in unsteady film cooling behaviors of gas turbine blades between mainstream and cooling air pulsations for a cylindrical hole
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Publisher
Elsevier BV
Reference36 articles.
1. Large Eddy Simulations of Discrete Hole Film Cooling With Plenum Inflow Orientation Effects;Acharya;J. Heat Transfer,2013
2. S. Baek, S. Yavuzkurt, Effects of oscillations in the main flow due to thermo acoustic fields in a gas turbine combustor on film cooling, Proceedings of ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition GT2016-56402.
3. Large eddy simulation of film cooling for a forward expansion hole under main flow oscillation;Baek;Int. J. Heat Mass Transf.,2024
4. Experimental investigation of the effects of blowing conditions and Mach number on the unsteady behavior of coolant ejection through a trailing edge cutback;Barigozzi;Int. J. Heat Fluid Flow,2012
5. Study of Unforced and Modulated Film-Cooling Jets Using Proper Orthogonal Decomposition-Part Ⅱ: Forced Jets;Bidan;J. Turbomach.,2013
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