Use of incompatible displacement modes for the calculation of element stiffnesses or stresses
Finite Elements in Analysis and Design
On the stability of mixed finite elements in large strain analysis of incompressible solids
Finite Elements in Analysis and Design
Towards improving the MITC6 triangular shell element
Computers and Structures
A 4-node 3D-shell element to model shell surface tractions and incompressible behavior
Computers and Structures
Detailed reliability assessment of triangular MITC elements for thin shells
Computers and Structures
The quadratic MITC plate and MITC shell elements in plate bending
Advances in Engineering Software
Measuring the convergence behavior of shell analysis schemes
Computers and Structures
An efficient meshfree method for vibration analysis of laminated composite plates
Computational Mechanics
An enriched 6-node MITC plate element for yield line analysis
Computers and Structures
The MITC3 shell finite element enriched by interpolation covers
Computers and Structures
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We present a triangular six-node shell element that represents an important improvement over a recently published element [1]. The shell element is formulated, like the original element, using the MITC procedure. The element has the attributes to be spatially isotropic, to pass the membrane and bending patch tests, to contain no spurious zero energy mode, and is formulated without an artificial constant. In particular, the improved element does not show the instability sometimes observed with the earlier published element. We give the convergence behavior of the element in discriminating membrane- and bending-dominated benchmark problems. These tests show the effectiveness of the element.