Conjugate heat transfer study of backdisc cooling of a radial turbine
Improving turbine endwall cooling uniformity by controlling near-wall secondary flows
Thermal imaging as flow visualization for gas-turbine film cooling
Results of conjugate modeling and analysis of the thermal state of a high-pressure turbine blade
Other Components of the Jet Engine
Steady computations of ingress through gas turbine rim seals
Performance analysis of an aero engine with inter-stage turbine burner