Equivalent single-layer theory for a complete stress field in sandwich panels under arbitrarily distributed loading

Composite Structures

Volumn 58, Issue 4, 2002, Pages 483-495

  Barut, A ^a   Madenci, E ^a   Anderson, T ^b   Tessler, A ^c  

^a University of Arizona   (United States)

^b UNIVERSITY OF WASHINGTON   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Fourier series; Sandwich; Single layer; Step loading; Virtual work

Indexed keywords

BOUNDARY CONDITIONS; KINEMATICS; SANDWICH STRUCTURES; STRESSES;

SINGLE-LAYER THEORY;

COMPOSITE MATERIALS;

LOADING; STRESS; THEORY;

EID: 0036893953     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00137-X     Document Type: Article

References (12)

1. On the theory of bending of elastic plates
2. The effect of transverse shear deformations on the bending of elastic plates
3. Influence of rotating inertia and shear on flexural motions of isotropic, elastic plates
4. A general non-linear third-order theory of plates with moderate thickness
5. Hierarchic models for laminated composites
6. A comprehensive analysis of the state of stress of elastic anisotropic flat plates using refined theories
7. A higher-order theory for plate deformation: Part 1. homogeneous plates; part 2. laminated plates
8. An improved plate theory of (1,2)-order for thick composite laminates
9. A (3,2)-order bending theory for laminated composite and sandwich beams
10. Analysis of thick sandwich construction by a (3,2)-order theory
11. Strain and stress computations in thick laminated plates using hierarchical higher-order kinematics
12. Analytical solution of finite-geometry composite panels under transient surface loading