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Buckling, shell element

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ExampleReferenceRecordsLargest deviation
Simply supported square plate, uniaxial compressionPublished source11.36%
Simply supported square plate, equal biaxial compressionPublished source11.36%

Problem. In a shell the geometric stiffness comes from the membrane forces. A square plate simply supported on four edges is tested under uniaxial and equal biaxial compression.

Reference document. Timoshenko & Gere, Theory of Elastic Stability, chapter nine, is used.

The critical membrane force of a square plate simply supported on all four edges is given by these relations for uniaxial and biaxial compression.

Ncr=4π2Db2  (uniaxial),Ncr=2π2Db2  (biaxial)N_{cr} = \dfrac{4\pi^2 D}{b^2}\ \ \text{(uniaxial)},\qquad N_{cr} = \dfrac{2\pi^2 D}{b^2}\ \ \text{(biaxial)}

Numerical model. The plate is modelled with ten by ten quadrilateral shell elements, and only the vertical translation is held on the edges. In the uniaxial case the in-plane restraint is given at a single node, so the Poisson expansion of the edge is not restrained.

Simply supported square plate, uniaxial compression

Parameters. mesh = 10×10 · b = 4 · t = 0.02

Published source. Timoshenko & Gere, with the coefficient taken as 4 for a square plate

Ncr=k π2D/b2N_{cr} = k\,\pi^2 D / b^2
QuantityReferenceComputedDeviation
Critical membrane force361.524366.4231.36%

Simply supported square plate, equal biaxial compression

Parameters. mesh = 10×10 · b = 4 · t = 0.02

Published source. Timoshenko & Gere, k=2k = 2 for a square plate under biaxial compression

QuantityReferenceComputedDeviation
Critical membrane force180.762183.2121.36%