A high fidelity composite bonded joint analysis validation study - Part I: Analysis

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2005, Pages 4436-4451

  Engelstad, S P ^a,e   Berry, O T ^a,e   Renieri, G D ^b,f   Deobald, L R ^b,f   Mabson, G E ^b,g   Dopker, B ^b,h   Nottorf, E W ^c,f   Clay, S B ^d  

^a LOCKHEED MARTIN   (United States)

^b BOEING COMPANY   (United States)

^c BELL HELICOPTER TEXTRON INC   (United States)

^d AIR FORCE RESEARCH LABORATORY   (United States)

^e Technology Development and Integration   (United States)

^f Composite Processes Phantom Works ^*

^g Phantom Works Structures Technology

^h 787 Fuselage Structural Test and Technology

Author keywords

[No Author keywords available]

Indexed keywords

BOND (MASONRY); COMPOSITE BEAMS AND GIRDERS; DATA ACQUISITION; DELAMINATION; FINITE ELEMENT METHOD; FRACTURE MECHANICS; STRUCTURAL ANALYSIS;

COMPOSITE BONDED JOINT ANALYSIS; COMPOSITES AFFORDABILITY INITIATIVE (CAI); DAMAGE TOLERANCE; FIDELITY ANALYSIS;

JOINTS (STRUCTURAL COMPONENTS);

EID: 28844480976     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2166     Document Type: Conference Paper

References (15)

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