An object oriented system for damage tolerance design of stiffened panels

Engineering Analysis with Boundary Elements

Volumn 23, Issue 1, 1999, Pages 21-34

  Salgado, N K ^a   Aliabadi, M H ^b  

^a Department of Engineering   (Brazil)

^b QUEEN MARY UNIVERSITY OF LONDON   (United Kingdom)

Author keywords

Aircraft stiffened panels; Boundary element method; Fracture mechanics; Knowledge based system

Indexed keywords

AIRCRAFT; BOUNDARY ELEMENT METHOD; COMPUTATIONAL GEOMETRY; CRACK PROPAGATION; FRACTURE MECHANICS; GRAPHICAL USER INTERFACES; INTERACTIVE COMPUTER SYSTEMS; KNOWLEDGE BASED SYSTEMS; OBJECT ORIENTED PROGRAMMING; RESIDUAL STRESSES;

AIRCRAFT STIFFENED PANELS; DAMAGE TOLERANCE DESIGN; INCREMENTAL CRACK EXTENSION ANALYSIS; USER-FRIENDLY WINDOWS-BASED INTERFACES;

STRUCTURAL PANELS;

EID: 0032762159     PISSN: 09557997     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0955-7997(98)00058-7     Document Type: Article

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