An experimental study of heat transfer in the rectangular coolant passages of a gas turbine rotor blade /

Modern gas turbines have high inlet temperatures to harness maximum power output, which causes different components to experience severe thermal stresses and fatigue. To achieve turbine blade durability goals, the blades are cooled with air extracted from the compressor. The amount of air to be extr...

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Bibliographic Details
Main Author: Uddin, Mohammed Jalal, 1971-
Format: Thesis eBook
Language:English
Published: [Place of publication not identified] : [publisher not identified] ; 2000.
Subjects:
Online Access:Link to OAKTrust copy

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Call Number: 2000 Thesis U43
 
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2000 Thesis U43 Available

Available Online

Holdings details from Available Online
Call Number: 2000 Thesis U43
 
Call Number Status Get It
2000 Thesis U43 Available