Jet impingement heat transfer in rotating coolant passages /

In gas turbine engines, increasing turbine inlet temperature increases engine thermal efficiency but also increases the amount of heat transferred to the turbine blades. To achieve reasonable turbine blade durability goals, the blades are cooled with air extracted from the compressor but at a penal...

Full description

Bibliographic Details

Main Author:	Parsons, James Auner
Format:	Thesis Book
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1995.
Subjects:	Major mechanical engineering.
Online Access:	Link to OAKTrust copy