Jet impingement cooling in rotating coolant passages of gas turbine blades /

Jet impingement cooling was studied in a simulated rotating gas turbine blade, focussing the effects of Coriolis and centrifugal forces on new impingement-cooling configurations. The experiments were performed on two test models, namely two-pass rotating rectangular channel and one-pass rotating rec...

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Bibliographic Details

Main Author:	Akella, Kumar Vyaghreswara, 1971-
Format:	Thesis Book
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1998.
Subjects:	Major mechanical engineering.
Online Access:	http://proxy.library.tamu.edu/login?url=http://proquest.umi.com/pqdweb?did=733038961&sid=1&Fmt=2&clientId=2945&RQT=309&VName=PQD