Numerical study on the influence of coolant temperature, pressure, and thermal barrier coating thickness on heat transfer in high-pressure blades
Duy-Tan Vo, Thanh Dam, Byung‐Wook Kim, Jaiyoung Ryu
Topics & Concepts
CoolantMaterials scienceTurbine bladeHeat transferThermal barrier coatingMechanicsThermodynamicsCoatingComposite materialTurbinePhysicsTurbomachinery Performance and OptimizationHeat Transfer MechanismsCombustion and flame dynamics