Assessment of cure-residual strains through the thickness of carbon-epoxy laminates using FBGs Part II: Technological specimen

Composites Part A: Applied Science and Manufacturing

Volumn 40, Issue 10, 2009, Pages 1534-1544

  Mulle, M ^a   Collombet, F ^a   Olivier, P ^a   Zitoune, R ^a   Huchette, C ^b   Laurin, F ^b   Grunevald, Y H ^c  

^a INSA   (France)

^b ONERA   (France)

^c Composites Expertise and Solutions ^*  (France)

Author keywords

A. Technological specimen; B. Residual internal stress; C. FBG sensors; D. Process monitoring

Indexed keywords

A. TECHNOLOGICAL SPECIMEN; AUTOCLAVE CURE; B. RESIDUAL/INTERNAL STRESS; C. FBG SENSORS; CARBON-EPOXY LAMINATES; CURE CYCLE; D. PROCESS MONITORING; ENVIRONMENTAL EFFECTS; FEM SIMULATIONS; HEATING TESTS; IN-PLANE; INDUCED STRAIN; MEASUREMENT PROCEDURES; NON-UNIFORM DISTRIBUTION; OPTICAL FIBRE; PROCESS-INDUCED STRAIN; REINFORCED ZONE; RESIDUAL STRAINS; STRUCTURAL ISSUES; THERMAL PROPERTIES; THERMALLY INDUCED STRAIN;

AUTOCLAVES; CURING; FIBER BRAGG GRATINGS; OPTICAL FIBERS; PROCESS CONTROL; PROCESS MONITORING; SENSORS; THERMODYNAMIC PROPERTIES;

PAPER LAMINATES;

EID: 70249134880     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesa.2009.06.013     Document Type: Article

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