Elastic-plastic wrinkling of compression loaded sandwich panels made with layered cores was studied analytically and experimentally. A core with a stiff layer near the sandwich skins can improve various properties, including wrinkling and impact strengths, with only a minor weight penalty. The 2D plane stress and plane strain bifurcation problems were solved analytically, save for a determinantal equation which was solved numerically. Experiments were performed on aluminum skin/foam core sandwich panels with different combinations of stiff and soft core materials. Good correlation between experiments and theory was obtained.
1.
Danielsson
, M.
, and Grenestedt
, J. L.
, 1998
, “Gradient Foam Core Materials for Sandwich Structures, Preparation and Characterisation
,” Composites, Part A
, 29
(8
), pp. 981
–988
.2.
Gough
, G. S.
, Elam
, C. F.
, and de Bruyne
, N. A.
, 1940
, “The Stabilization of a Thin Sheet by a Continuous Supporting Medium
,” J. R. Aeronaut. Soc.
, 44
, pp. 12
–43
.3.
Hoff
, N. J.
, and Mautner
, S. E.
, 1945
, “The Buckling of Sandwich-Type Panels
,” J. Aeronaut. Sci.
, 12
, pp. 285
–297
, eq. (103).4.
Grenestedt, J. L., and Olsson, K.-A., 1995, “Wrinkling of Sandwich with Layered Core or Non-Symmetric Skins,” Proc. Third International Conference on Sandwich Construction, Southampton, UK, 12–15 September.
1.
Shield
, T. W.
, Kim
, K. S.
, and Shield
, R. T.
, 1994
, “The Buckling of an Elastic Layer Bonded to an Elastic Substrate in Plane Strain
,” ASME J. Appl. Mech.
, 61
, pp. 231
–235
. 2.
Corrections: ASME J. Appl. Mech., 61, pp. 796, and further, 1994, b=ω[1−P1−2ν/2μ1−ν]1/2 in Eq. (4).
1.
Hill
, R.
, 1957
, “On Uniqueness and Stability in the Theory of Finite Elastic Strains
,” J. Mech. Phys. Solids
, 5
, pp. 229
–241
.2.
Hill
, R.
, 1967
, “Eigenmodal Deformations in Elastic/Plastic Continua
,” J. Mech. Phys. Solids
, 15
, pp. 371
–386
.3.
Hutchinson, J. W., 1974, “Plastic Buckling,” in Advances in Applied Mechanics, C.-S. Yih, ed., 14, pp. 67–144.
4.
DIAB. Divinycell H-Grade Technical Manual, 10.00. DIAB AB, Box 201, S-312 22 Laholm, Sweden (also available at www.diabgroup.com/DIAB/filecabinet.nsf/LookupFiles/H_Man_M/$file/H_Man_M.pdf)
5.
Ley, R. P., Lin, W., and Mbanefo, U., 1999, “Facesheet Wrinkling in Sandwich Structures,” NASA/CR-1999-208994.
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