Stress analysis of turbine components under spin rig thermomechanical condition
This paper presents the stress analysis of a second stage turbine disc, subjected to spin rig test. To solve the problem, the finite element analysis of complex geometrical model of the disc/blade segment with much physical nonlinearity such as contact and plasticity was carried out. The adequate m...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2004-12-01
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| Series: | Aviation |
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| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/7477 |