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The Influence of Film Cooling and Inlet Temperature Profile on Heat Transfer for the Vane Row of a 1-1/2 Stage Transonic High-Pressure Turbine

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1. http://rave.ohiolink.edu/etdc/view?acc_num=osu1284261128

Identifer	oai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:osu1284261128
Date	01 November 2010
Creators	Kahveci, Harika Senem
Publisher	The Ohio State University / OhioLINK
Source Sets	Ohiolink ETDs
Language	English
Detected Language	English
Type	text
Source	http://rave.ohiolink.edu/etdc/view?acc_num=osu1284261128
Rights	unrestricted, This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.