An Enhanced Flow-Thermo-Structural Modeling and Validation for the Integrated Analysis of a Film Cooling Nozzle Guide Vane
The target of this paper is to develop an enhanced flow-thermo-structural (FTS) model with high computational accuracy, to perform the integrated analysis of film cooling nozzle guide vane (NGV).An efficient turbulence model and weak spring approach are utilized in the enhanced FTS model.In respect of the power balance principle of aeroengine rotor