Deformation of antisymmetric laminate under centrifugal force and/or thermal load

Composite Structures

Volumn 51, Issue 4, 2001, Pages 335-344

  Zhou, Fenghua ^a   Ogawa, Akinori ^a   Hashimoto, Ryosaku ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Antisymmetric laminate; Follower force; Large strain; Rayleigh Ritz method; Smart blade; Stretching twisting coupling; Structural nonlinearity

Indexed keywords

DEFORMATION; FINITE ELEMENT METHOD; THERMAL LOAD;

CENTRIFUGAL FORCE;

LAMINATES;

CENTRIFUGAL FORCE; COMPUTER SIMULATION; DEFORMATION; INDUSTRIAL TEXTILE; LAMINATE; MATHEMATICAL ANALYSIS;

EID: 0035310043     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00149-5     Document Type: Article

References (15)

1. On the smart blade structures of aeroengine compressors
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4. The room-temperature shapes of four-layer unsymmetric cross-ply laminates
5. Non-linear temperature-curvature relationships for unsymmetric graphite-epoxy laminates
6. Cured shape of unsymmetric laminates with arbitrary layup angles
7. Thermal deformation of anti-symmetric laminates at cure
8. The room-temperature shape of general unsymmetric laminates
9. Thermal-induced deformation behavior of unsymmetric laminates
10. Advanced calculation of the room-temperature shapes of thin unsymmetric composite laminates
11. Advanced calculation of the room-temperature shapes of unsymmetric laminates
12. Evaluation of static strength of T800H/PMR-15 Carbon/Polyimide laminates at room temperature and 300°C