There exist many formulas for the critical compression of sandwich plates, each based on a specific set of assumptions and a specific plate or beam model. It is not easy to determine the accuracy and range of validity of these rather simple formulas unless an elasticity solution exists. In this paper, we present an elasticity solution to the problem of buckling of sandwich beams or wide sandwich panels subjected to axially compressive loading (along the short side). The emphasis on this study is on the wrinkling (multi-wave) mode. The sandwich section is symmetric and all constituent phases, i.e., the facings and the core, are assumed to be orthotropic. First, the pre-buckling elasticity solution for the compressed sandwich structure is derived. Subsequently, the buckling problem is formulated as an eigen-boundary-value problem for differential equations, with the axial load being the eigenvalue. For a given configuration, two cases, namely symmetric and anti-symmetric buckling, are considered separately, and the one that dominates is accordingly determined. The complication in the sandwich construction arises due to the existence of additional “internal” conditions at the face sheet∕core interfaces. Results are produced first for isotropic phases (for which the simple formulas in the literature hold) and for different ratios of face-sheet vs core modulus and face-sheet vs core thickness. The results are compared with the different wrinkling formulas in the literature, as well as with the Euler buckling load and the Euler buckling load with transverse shear correction. Subsequently, results are produced for one or both phases being orthotropic, namely a typical sandwich made of glass∕polyester or graphite∕epoxy faces and polymeric foam or glass∕phenolic honeycomb core. The solution presented herein provides a means of accurately assessing the limitations of simplifying analyses in predicting wrinkling and global buckling in wide sandwich panels∕beams.

1.
Hoff
,
N. J.
, and
Mautner
,
S. F.
, 1945, “
The Buckling of Sandwich-Type Panels
,”
J. Aeronaut. Sci.
0095-9812,
12
, pp.
285
297
.
2.
Goodier
J. N.
, and
Neou
I. M.
, 1951, “
The Evaluation of Theoretical Compression in Sandwich Plates
,”
J. Aeronaut. Sci.
0095-9812,
18
, pp.
649
657
.
3.
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.
0368-3931,
44
, pp.
12
43
.
4.
Allen
,
H. G.
, 1969,
Analysis and Design of Structural Sandwich Panels
,
Pergamon
, Oxford, UK, Chap. 8.
5.
Birman
,
V.
, and
Bert
,
C. W.
, 2002, “
Wrinkling of Composite-Facing Sandwich Panels Under Biaxial Loading
,”
IMECE 02, the 2002 International Mechanical Engineering Congress & Exposition
, November 17–22,
New Orleans
, LA.
6.
Kardomateas
,
G. A.
, 1993, “
Buckling of Thick Orthotropic Cylindrical Shells Under External Pressure
,”
ASME J. Appl. Mech.
0021-8936,
60
, pp.
195
202
.
7.
Kardomateas
,
G. A.
, and
Chung
,
C. B.
, 1994, “
Buckling of Thick Orthotropic Cylindrical Shells Under External Pressure Based on Non-Planar Equilibrium Modes
,”
Int. J. Solids Struct.
0020-7683
31
, pp.
2195
2210
.
8.
Kardomateas
,
G. A.
, 1993, “
Stability Loss in Thick Transversely Isotropic Cylindrical Shells Under Axial Compression
,”
ASME J. Appl. Mech.
0021-8936,
60
, pp.
506
513
.
9.
Kardomateas
,
G. A.
, 1995, “
Bifurcation of Equilibrium in Thick Orthotropic Cylindrical Shells Under Axial Compression
,”
ASME J. Appl. Mech.
0021-8936,
62
, pp.
43
52
.
10.
Soldatos
,
K. P.
, and
Ye
,
J-Q.
, 1994, “
Three-Dimensional Static, Dynamic, Thermoelastic and Buckling Analysis of Homogeneous and Laminated Composite Cylinders
,”
Compos. Struct.
0263-8223,
29
, pp.
131
-
143
.
11.
Kardomateas
,
G. A.
, and
Simitses
,
G. J.
, 2005, “
Elasticity Solution for the Bucking of Long Sandwich Cylindrical Shells Under External Pressure
,”
ASME J. Appl. Mech.
0021-8936,
72
, pp.
493
499
.
12.
Lekhnitskii
,
S. G.
, 1963,
Theory of Elasticity of an Anisotropic Elastic Body
, Holden Day, San Francisco (also
Mir Publishers
, Moscow, 1981).
13.
Kardomateas
,
G. A.
, 2001, “
Elasticity Solutions for a Sandwich Orthotropic Cylindrical Shell Under External Pressure, Internal Pressure and Axial Force
,”
AIAA J.
0001-1452
39
, pp.
713
719
.
14.
Novozhilov
,
V. V.
, 1953,
Foundations of the Nonlinear Theory of Elasticity
,
Graylock
, Rochester, NY.
15.
Press
,
W. H.
,
Flannery
,
B. P.
,
Teukolsky
,
S. A.
, and
Vetterling
,
W. T.
, 1989,
Numerical Recipes
,
Cambridge University Press
, Cambridge.
16.
Plantema
,
F. J.
, 1966,
Sandwich Construction
,
John Wiley & Sons
, New York.
17.
Vonach
,
W. K.
, and
Rammerstorfer
,
F. G.
, 2000, “
Wrinkling of Thick Orthotropic Sandwich Plates under General Loading Conditions
,”
Arch. Appl. Mech.
0939-1533
70
, pp.
338
348
.
18.
Grenestedt
,
J. L.
, and
Olsson
,
K.-A.
, 1995,
Proc., Third International Conference on Sandwich Construction
,
Southampton
, U.K., 12–15 September.
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