Heat transfer investigation in new cooling schemes of a stationary blade trailing edge

Beniaiche, A.Ghenaiet, A.Carcasci, C.Facchini, B.2015-10-292015-10-29201513594311https://dspace.univ-boumerdes.dz/handle/123456789/2363enHeat transfer coefficientNusselt numberPedestalsRibsStationary gas turbine bladeTLC techniqueTrailing edge cooling schemesHeat transfer investigation in new cooling schemes of a stationary blade trailing edgeArticle