A theoretical approach for evaluating the plane strain fracture toughness of ductile metals
- Author
- FARAHMAND, B1 ; BOCKRATH, G. E1
[1] Space Station Division, McDonnell Douglas Aerospace, 5301 Bolsa Avenue, Huntington Beach, CA 92646, United States - Source
Engineering fracture mechanics. 1996, Vol 53, Num 6, pp 975-990 ; ref : 14 ref
- CODEN
- EFMEAH
- ISSN
- 0013-7944
- Scientific domain
- Mechanics acoustics; Metallurgy, welding
- Publisher
- Elsevier, Oxford
/
Elsevier, Tarrytown, NY
- Publication country
- United Kingdom
- Document type
- Article
- Language
- English
- Keyword (fr)
- Alliage base aluminium Champ déformation Déformation plane Etude théorique Extrémité fissure Matériau ductile Mécanique rupture Relation contrainte déformation Ténacité Alliage Al
- Keyword (en)
- Aluminium base alloys Strain distribution Plane strain Theoretical study Crack tip Ductile material Fracture mechanics Stress strain relation Fracture toughness
- Keyword (es)
- Campo deformación Deformación plana Estudio teórico Extremidad fisura Material dúctil Mecánica ruptura Relación tensión deformación Tenacidad
- Keyword (de)
- Zweiachsige Verformung Theoretische Untersuchung Bruchmechanik Bruchzaehigkeit
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D11 Metals. Metallurgy / 001D11G Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology / 001D11G05 Fractures
- Discipline
- Metals. Metallurgy
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 3011874
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
10.1016/0013-7944(95)00139-5 
https://dx.doi.org/10.1016/0013-7944(95)00139-5
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