Analysis of burst margin and critical speed of gas turbine disc for aeroengine application

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PH1727.pdf (5.96 MB)
Date
2021-03
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Publisher
Indian Institute of Technology (Indian School of Mines), Dhanbad
Abstract
Description
Keywords
Gas turbine disc, Burst speed, Aircraft gas turbine engine, Burst margin, Ph.D, MECH, PH1727
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http://hdl.handle.net/123456789/1937
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Sanjoy Kumar Ghoshal