QR Code

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:
Détails bibliographiques
Auteurs principaux: Yuriy Nyashin, Victor Shishlyaev
Format: Artigo
Langue:Inglês
Publié: Wiley 1998-01-01
Collection:International Journal of Rotating Machinery
Sujets:
Accès en ligne:http://dx.doi.org/10.1155/S1023621X98000219
Tags: Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!