Testing and analysis of ultra thick composites

Composites Part B: Engineering

Volumn 41, Issue 4, 2010, Pages 326-336

  Zimmermann, K ^a   Zenkert, D ^b   Siemetzki, M ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

A. Carbon carbon composites; C. Finite element analysis (FEA); Ultra thick laminates

Indexed keywords

3-D MODELING; BRICK ELEMENTS; CORRECTION FACTORS; CROSS SECTION; DISCRETISATION; FE METHOD; FINITE ELEMENT ANALYSIS; FULL SCALE; LANDING GEAR; MATERIAL THICKNESS; MOULD MANUFACTURING; MULTIPLE ELEMENTS; MULTIPLE LOAD CASE; NORMAL STRESS; OUT-OF PLANE; SOLID COMPOSITES; STRESS GRADIENT; STRESS VARIATIONS; TEST PROGRAM; TEST RESULTS; THICK COMPOSITES; THICK LAMINATES; TRANSVERSE SHEAR;

AIRCRAFT LANDING SYSTEMS; CARBON CARBON COMPOSITES; CARBON FIBERS; FINITE ELEMENT METHOD; LAMINATES; LANDING GEAR (AIRCRAFT); PLASTICS; THREE DIMENSIONAL;

CARBON FIBER REINFORCED PLASTICS;

EID: 77951298968     PISSN: 13598368     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesb.2009.12.004     Document Type: Article

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