Fretting fatigue life analysis for a gas turbine compressor blade-disk material combination
In order to analyse fretting fatigue life of dove-tail joints used in the compressor stage of a gas turbine, experimental study of different material combinations was conducted using rectangular fatigue specimen and bridge type pads. Specimen and pad interaction was simulated numerically and obtaine...
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| Format: | Others |
| Language: | English |
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KTH, Hållfasthetslära
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-284357 |