Analytic Creep Durability of Rotating Uniform Disks
Turbine disks of aircraft engines in operation are subjected to alternating thermocyclic deformation under high temperatures. Operation gives rise to sufficiently high stresses and subsequent creep damaging effects.
Enregistré dans:
| Auteurs principaux: | , |
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| Format: | Artigo |
| Langue: | Inglês |
| Publié: |
Wiley
1998-01-01
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| Collection: | International Journal of Rotating Machinery |
| Sujets: | |
| Accès en ligne: | http://dx.doi.org/10.1155/S1023621X98000219 |
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