Numerical Study of Aerodynamic Losses of Effusion Cooling Holes in Aero-Engine Combustor Liners
Journal of engineering for gas turbines and power ; 133 , 2 ; 21901-21902
2011
Aufsatz (Zeitschrift)
Englisch
Unsteady CFD investigation of effusion cooling process in a lean burn aero-engine combustor
Online Contents | 2016
|Experimental Study of Impingement Effusion-Cooled Double-Wall Combustor Liners: Thermal Analysis
DataCite | 2021
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