Hybrid titanium-CFRP laminates for high-performance bolted joints

Composites Part A: Applied Science and Manufacturing

Volumn 40, Issue 12, 2009, Pages 1826-1837

  Camanho, P P ^a   Fink, A ^b   Obst, A ^c   Pimenta, S ^d  

^a UNIVERSITY OF PORTO   (Portugal)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c EUROPEAN SPACE AGENCY   (Netherlands)

^d UNIVERSITY OF PORTO   (Portugal)

Author keywords

B. Strength; C. Finite element analysis; D. Mechanical testing; E. Joints joining

Indexed keywords

B. STRENGTH; CFRP LAMINATE; CFRP STRUCTURES; COHESIVE ELEMENT; E. JOINTS/JOINING; FAILURE MECHANISM; FINITE ELEMENT ANALYSIS; HYBRID COMPOSITE LAMINATE; HYBRID COMPOSITES; HYBRID LAMINATES; MECHANICAL RESPONSE; MODELING STRATEGY; NONLINEAR FINITE ELEMENT METHOD; NUMERICAL INVESTIGATIONS; NUMERICAL MODELS; PLANE STRESS; THREE DIMENSIONAL FINITE ELEMENT MODEL; TRANSITION REGIONS;

BEARINGS (STRUCTURAL); BOLTED JOINTS; BOLTS; HYBRID MATERIALS; MECHANICAL ENGINEERING; MECHANICAL TESTING; PAPER LAMINATES; THREE DIMENSIONAL; TITANIUM;

FINITE ELEMENT METHOD;

EID: 71649100159     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesa.2009.02.010     Document Type: Article

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