Finite element modeling of mechanically fastened composite-aluminum joints in aircraft structures

Composite Structures

Volumn 109, Issue 1, 2014, Pages 198-210

  Kapidžić, Zlatan ^a,b   Nilsson, Larsgunnar ^b   Ansell, Hans ^a  

^a SAAB AB   (Sweden)

^b LINKÖPING UNIVERSITY   (Sweden)

Author keywords

Bolted joints; Composite aluminum; Finite element modeling; Hybrid wing structures

Indexed keywords

AIRCRAFT MANUFACTURE; AIRFRAMES; ALUMINUM; BOLTED JOINTS; FINITE ELEMENT METHOD; LOADING; LOCKS (FASTENERS);

COMPOSITE-ALUMINUM; FORCE-DISPLACEMENT CHARACTERISTICS; FORCE-DISPLACEMENT RESPONSE; INCREASED TEMPERATURE; NON-LINEAR RESPONSE; TEMPERATURE DIFFERENCES; ULTIMATE FAILURE LOADS; WING STRUCTURES;

STRUCTURAL DESIGN;

EID: 84890885784     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2013.10.056     Document Type: Article

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