Blade tip clearance effect on the performance and flow field of a three stage axial turbine /

The effect of a 1.5 % blade tip clearance on a rotating three stage turbine under different operating points was investigated using radially and circumferentially traversed five hole pressure probes. The probes were used to obtain flow field total and static pressures, absolute and relative velociti...

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Bibliographic Details

Main Author:	Abdel-Fattah, Sharef Aly, 1978-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2003.
Subjects:	Major mechanical engineering.
Online Access:	Link to OAKTrust copy