Feasible region in general design space of lamination parameters for laminated composites

AIAA Journal

Volumn 40, Issue 3, 2002, Pages 559-565

  Diaconu, Cezar Gabriel ^a   Sato, Masaki ^a   Sekine, Hideki ^a  

^a TOHOKU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

LAMINATING; OPTIMIZATION; PARAMETER ESTIMATION; SHEAR DEFORMATION; STIFFNESS;

LAMINATION PARAMETERS;

LAMINATED COMPOSITES;

EID: 0036493820     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1683     Document Type: Article

References (18)

1. Stability optimization of laminated composite plates under in-plane loads
2. Material design of composite laminates with required in-plane elastic properties
3. Design of laminated fibrous composite plates with required flexural stiffness
4. On laminated configurations for simultaneous failure
5. Simplified design techniques for laminated cylindrical pressure vessels under stiffness and strength constraints
6. Stiffness optimization of orthotropic laminated composite s using lamination parameters
7. Layup optimization of composite material structures
8. Stiffness design method of symmetric laminates using lamination parameters
9. Material design of laminated fibrous composites with required bending-twisting coupling
10. Layup optimization against buckling of shear panels
11. Optimal design of symmetric laminated plates for fundamental frequency
12. Buckling design of symmetrically laminated plates using lamination parameters
13. Parameterization in laminate design for optimal compliance
14. Lamination parameters for reissner-mindlin plates
15. A general approach forcing convexity of ply angle optimization in composite laminates
16. A procedure for designing laminated plates with required stiffness properties. Application to thin quasi-isotropic quasi-homogeneous uncoupled laminates