Compression facing wrinkling of composite sandwich structures

Mechanics of Materials

Volumn 35, Issue 3-6, 2003, Pages 511-522

  Gdoutos, E E ^a   Daniel, I M ^a   Wang, K A ^a  

^a Northwestern University   (United States)

Author keywords

Core failure; Foam core; Sandwich beams; Sandwich columns; Sandwich structures; Wrinkling failure

Indexed keywords

ALUMINUM; BENDING (DEFORMATION); CANTILEVER BEAMS; COMPOSITE STRUCTURES; COMPRESSION TESTING; ELASTIC MODULI; HONEYCOMB STRUCTURES; INDENTATION; STIFFNESS;

SANDWICH BEAMS;

SANDWICH STRUCTURES;

EID: 0037342161     PISSN: 01676636     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-6636(02)00267-3     Document Type: Conference Paper

References (26)

1. Allen H.G. Analysis and Design of Structural Sandwich Panels. 1969;Pergamon, London.
2. Benson A.S., Mayers J. General instability and face wrinkling of sandwich plates - unified theory and applications. AIAA J. 5:1967;729-739.
3. Cox, H.L., 1945. Sandwich construction and core materials. Part III: Instability of sandwich struts and beams. Tech. Rep. R & M No. 2125, Aeronautical Research Committee.
4. Daniel I.M., Abot J.L. Fabrication testing and analysis of composite sandwich beams. Comput. Sci. Technol. 60:2000;2455-2463.
5. Daniel, I.M., Gdoutos, E.E., Wang, K.-A., Abot, J.L., 2001. Failure modes of composite sandwich beams, Int. J. Damage Mech., in press.
6. Ditcher A.K., Webber J.P.H. Non-linear stress-strain effects in the flexural wrinkling of carbon fibre honeycomb sandwich beams. Aeronaut. Quart. 33:1982;1-24.
7. Gdoutos E.E., Daniel I.M., Wang K.-A. Multiaxial characterization and modeling of a PVC cellular foam. J. Ther. Comp. Mat. 14:2001a;365-373.
8. Gdoutos E.E., Daniel I.M., Wang K.-A., Abot J.L. Nonlinear behavior of composite sandwich beams in three-point bending. Exp. Mech. 41:2001b;182-188.
9. Gdoutos E.E., Daniel I.M., Wang K.-A. Failure of cellular foams under multiaxial loading. Composites Part A. 33:2002a;163-176.
10. Gdoutos, E.E., Daniel, I.M., Wang, K.-A., 2002b. Indentation failure in composite sandwich structures. Exp. Mech., to appear.
11. Goodier J.N., Neou I.M. The evaluation of theoretical critical compression in sandwich plates. J. Aeronaut. Sci. 18:1951;649-657.
12. Gough G.S., Elam C.F., De Bruyne N.D. The stabilization of a thin sheet by a continuous supporting medium. J. Roy. Aeronaut. Soc. 44:1940;12-43.
13. Gutierrez A.J., Webber J.P.H. Flexural wrinkling of honeycomb sandwich beams with laminated faces. Int. J. Sol. Struct. 16:1980;645-651.
14. Hadi B.K., Matthews F.L. Development of Benson-Mayers theory on the wrinkling of anisotropic sandwich panels. Comput. Struct. 49:2000;425-434.
15. Heath W.G. Sandwich construction, Part 2: The optimum design of flat sandwich panels. Aircraft Eng. 32:1960;230-235.
16. Hoff N.J., Mautner S.E. The buckling of sandwich-type panels. J. Aero. Sci. 12:1945;285-297.
17. Hunt G.W., Wadee M.A. Localization and mode interaction in sandwich structures. Proc. Roy. Soc. Lon. A. 454:1968;1197-1216.
18. Niu K., Talreja R. Modeling of wrinkling in sandwich panels under compression. J. Eng. Mech. 125:1999;875-883.
19. Pearce T.R.A., Webber J.P.H. Buckling of sandwich panels with laminated faceplates. Aeronaut. Quart. 23:1972;148-160.
20. Pearce T.R.A., Webber J.P.H. Experimental buckling loads of sandwich panels with carbon fibre faceplates. Aeronaut. Quart. 24:1973;295-312.
21. Plantema F.J. Sandwich Constructions. 1966;Wiley, New York.
22. Stiftinger M.A., Rammerstorfer F.G. Face layer wrinkling in sandwich shells - theoretical and experimental investigations. Thin-Walled Struct. 29:1997;113-127.
23. Vonach W.K., Rammerstorfer F.G. The effect of in-plane core stiffness on the wrinkling behavior of thick sandwiches. Acta Mech. 141:2000a;1-10.
24. Vonach W.K., Rammerstorfer F.G. Wrinkling of thick orthotropic sandwich plates under general loading conditions. Arch. Appl. Mech. 70:2000b;338-348.
25. Wadee M.A., Hunt G.W. Interactively induced localized buckling in sandwich structures with core orthotropy. J. Appl. Mech., Trans. ASME. 65:1998;523-528.
26. Webber J.P.H., Kyriakides S., Lee C.T. On the wrinkling of honeycomb sandwich columns with laminated cross-ply faces. Aeronaut. J. 80:1976;264-272.