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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DOI
10.1016/0020-7403(95)00063-1 
https://dx.doi.org/10.1016/0020-7403(95)00063-1
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