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Prediction of creep failure in aeroengine materials under multi-axial stress states

Author
HYDE, T. H; XIA, L; BECKER, A. A
Univ. Nottingham, dep. mechanical eng., Nottingham NG7 2RD, United Kingdom
Source

International journal of mechanical sciences. 1996, Vol 38, Num 4, pp 385-403, 18 p ; ref : 15 ref

CODEN
IMSCAW
ISSN
0020-7403
Scientific domain
Mechanics acoustics; Metallurgy, welding
Publisher
Elsevier, Oxford
Publication country
United Kingdom
Document type
Article
Language
English
Keyword (fr)
Alliage Barre Contrainte axiale Endommagement Eprouvette entaillée Etude expérimentale Fluage Haute température Méthode numérique Méthode élément fini Nickel Prédiction Rupture Superalliage Symétrie axiale Titane alliage
Keyword (en)
Alloys Bar Axial stress Damaging Notched test piece Experimental study Creep High temperature Numerical method Finite element method Nickel Prediction Rupture Superalloy Axial symmetry Titanium alloy
Keyword (es)
Aleación Barra Tensión axial Deterioración Probeta entallada Estudio experimental Fluencia Alta temperatura Método numérico Método elemento finito Niquel Predicción Ruptura Superaléación Simetría axial Titanio aleación
Keyword (de)
Legierung Kerbpruefkoerper Experimentelle Untersuchung Kriechen Hochtemperatur Finite Element Methode Nickel Bruch Superlegierung Titanlegierung
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D11 Metals. Metallurgy / 001D11G Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology / 001D11G04 Creep

Discipline
Metals. Metallurgy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
2971714

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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