Knowledge based design method for fibre metal laminate fuselage panels

Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference - DETC2005

Volumn 2 B, Issue , 2005, Pages 699-708

  Vermeulen, B ^a   Van Tooren, M J L ^a   Peeters, L J B ^b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Glare Projects   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; AUTOMATION; KNOWLEDGE BASED SYSTEMS; LAMINATES;

COST REDUCTION; CURRENT DESIGN PROCESS; DESIGN PROCESS;

FUSELAGES;

EID: 33144477342     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/detc2005-84079     Document Type: Conference Paper

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