Analysis of the residual strength and link-up stress of aluminium plates with multi-site damage

11th International Conference on Fracture 2005, ICF11

Volumn 1, Issue , 2005, Pages 41-46

  Ciliato, G D ^a   Carneiro, S H S ^a  

^a INSTITUTO DE ESTUDOS AVANÇADOS   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

AERONAUTICAL STRUCTURES; ALUMINIUM PLATES; BASIC HYPOTHESIS; BOEING 737; CRACK TIP OPENING ANGLE; DUCTILE MATERIALS; ELASTOPLASTIC FRACTURE MECHANICS; INTERNATIONAL SPACE STATIONS; MULTI-SITE; PLASTIC ZONES; PRELIMINARY DESIGN; REASONABLE ACCURACY; RESIDUAL STRENGTH; SCIENTIFIC COMMUNITY; STIFFENED PANEL; STRUCTURAL COMPONENT; STRUCTURAL ELEMENTS;

AERODYNAMICS; ALUMINUM; CRACK TIPS; CRACKS; FRACTURE; FRACTURE MECHANICS; FUSELAGES; NASA;

AIRCRAFT ACCIDENTS;

EID: 84869854572     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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