Bird-strike simulation for certification of the Boeing 787 composite moveable trailing edge

Composite Structures

Volumn 86, Issue 1-3, 2008, Pages 258-268

  Georgiadis, Steve ^a   Gunnion, Andrew J ^b   Thomson, Rodney S ^b   Cartwright, Bruce K ^c  

^a Hawker de Havilland   (Australia)

^b Cooperative Research Centre for Advanced Composite Structures Ltd ^*  (Australia)

^c Pacific Engineering Systems International Pty Ltd   (Australia)

Author keywords

Bird strike; Carbon epoxy structures; Certification; Explicit analysis; Material models

Indexed keywords

ARCHITECTURAL ACOUSTICS; ARCHITECTURAL DESIGN; CARBON; CARBON FIBERS; COMPUTER SOFTWARE; DATA STRUCTURES; FINITE DIFFERENCE METHOD; FLUID DYNAMICS; FLUID MECHANICS; MATHEMATICAL MODELS; MODAL ANALYSIS; PAINTING; STRUCTURAL DESIGN; STRUCTURAL PANELS;

BIRD STRIKES; BOEING 787; CARBON-FIBRE EPOXY COMPOSITES; CERTIFICATION COSTS; DESIGN EFFICIENCY; ELSEVIER (CO); FINITE ELEMENT SOFTWARE (MARC2000); SIMULATION METHODOLOGY; SMOOTH PARTICLE HYDRODYNAMIC (SPH); TEST DATA; TRAILING EDGES;

FINITE ELEMENT METHOD;

AIRCRAFT; CARBON FIBER; COMPUTER SIMULATION; FIBER REINFORCED COMPOSITE; FINITE ELEMENT ANALYSIS; SOFTWARE; TESTING;

EID: 46749115109     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2008.03.025     Document Type: Article

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