Thermo-mechanical Behaviour of Turbine Disc Assembly in the Presence of Residual Stresses
A comprehensive three dimensional coupled thermo-mechanical finite element study is performed on turbine blade attachments in gas turbine engines. The effects of the self-generated centrifugal forces of the disc and the associated blades, thermal loads, and shot peening residual are all considered i...
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| Language: | en_ca |
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2013
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| Online Access: | http://hdl.handle.net/1807/43135 |