High-order bending of sandwich beams with a transversely flexible core and unsymmetrical laminated composite skins

Composites Engineering

Volumn 5, Issue 4, 1995, Pages 405-414

  Frostig, Y ^a   Shenhar, Y ^b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b ISRAEL AIRCRAFT INDUSTRIES   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000081069     PISSN: 09619526     EISSN: None     Source Type: Journal    
DOI: 10.1016/0961-9526(95)93440-7     Document Type: Article

References (24)

1. Structural analog for sandwich panels with finite deflections
2. Comparison of elasticity and sandwich theories for a rectangular sandwich plate
3. Behavior of delaminated sandwich beams with transversely flexible core-high order theory
4. On stress concentration in the bending of sandwich beams with a transversely flexible core
5. Bending of sandwich beams with transversely flexible core and transverse diaphragms
6. Bending of sandwich beam wth transversely flexible core
7. Buckling of simply-supported sandwich beams with transversely flexible core-a high order theory
8. Vibration of sandwich beams-a high order theory approach
9. Sandwich beams with unsymmetrical skins and a flexible core-bending behavior
10. A high order theory for the bending of sandwich beams with a flexible core
11. A new theory for bending of thick sandwich beams
12. Exact solutions to some honeycomb sandwich beam, plate, and shell problems
13. Interactive bending behavior of sandwich beams
14. Bending and vibration of CFRP-faced rectangular sandwich plates
15. Analysis of sandwich plates with unbalanced cross-ply faces
16. Modified stiffness formulation of unbalanced anisotropic sandwich plates
17. Stress analysis of sandwich plates with unidirectional thickness variation
18. Bending of sandwich plates of variable thickness
19. Behavior of sandwich beam with composite materials laminated skins and a “soft” core
20. Failure mode maps for foam core sandwich beams