Buckling loads of CFRP composite cylinders under combined axial and torsion loading - experiments and computations

Composite Structures

Volumn 53, Issue 4, 2001, Pages 427-435

  Meyer Piening, H R ^a   Farshad, M ^b   Geier, B ^c   Zimmermann, R ^c  

^a ETH ZURICH   (Switzerland)

^b SWISS FEDERAL LABORATORIES FOR MATERIALS SCIENCE AND TECHNOLOGY   (Switzerland)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Buckling analysis; Composites; Imperfection sensitivity; Shells

Indexed keywords

BUCKLING; CARBON FIBER REINFORCED PLASTICS; CYLINDERS (CONTAINERS); PHOTOGRAMMETRY; TORSIONAL STRESS;

LASER SCANNING;

COMPOSITE STRUCTURES;

BUCKLING; CARBON FIBER; FIBER REINFORCED COMPOSITE; LOADING;

EID: 0035451802     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00053-8     Document Type: Article

References (3)

1. Buckling tests with axially compressed unstiffened cylindrical shells made from CFRP
2. Some simple solutions for buckling loads of thin and moderately thick cylindrical shells and panels made of laminated composite material
3. Buckling and post-buckling of anisotropic shells