Measurement and analysis of gas turbine blade tip heat transfer /

To achieve higher thermal efficiency and thrust modern gas turbine engines operate at high combustor outlet temperatures of 1300-1500C. Turbine blades are exposed to these high temperature gases and undergo severe thermal stress and fatigue. Blade tips are the most critical regions, typically diff...

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Bibliographic Details

Main Author:	Azad, GM Salam
Format:	Thesis Book
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2000.
Subjects:	Major mechanical engineering.
Online Access:	http://proxy.library.tamu.edu/login?url=http://proquest.umi.com/pqdweb?did=727726091&sid=1&Fmt=2&clientId=2945&RQT=309&VName=PQD