Product: ABAQUS/Standard
Linear elastic, Young's modulus = 30 × 106, Poisson's ratio = 0.3, no piezoelectric coupling, isotropic dielectric constant 1.0 × 10–3.
Boundary conditions:
0, 
0.
Loading:
Distributed pressure of 1000/length on each edge.
Equivalent concentrated shear forces corresponding to distributed shear loading of 1000/length on each edge in the directions shown.
Distributed charges of 1000/length on each edge.
Concentrated charges at each node to negate the distributed charges, except for the distributed charge of 1000/length on the top surface.
Stresses
Both plane stress and plane strain elements,
–1000;
and for plane strain elements,
–600.
Strains
Plane strain elements,
–1.7333 × 10–5, 
–8.6667 × 10–5.
Plane stress elements,
–2.3333 × 10–5, –8.6667 × 10–5.
Electrical fluxes
Both plane stress and plane strain elements, 
0, 
–1000.
Electrical potential gradients
Both plane stress and plane strain elements, 
0, 
–1.0 × 106.
Displacements
, 
.
Potentials
.
Elements using reduced integration may have additional boundary conditions to those specified above. All elements yield exact solutions.
The *SECTION FILE and *SECTION PRINT output requests are used in some of the input files to output accumulated quantities on the face in the 
–
plane.
CPS3E elements.
CPS4E elements.
CPS6E elements.
CPS8E elements.
CPS8RE elements.
CPE3E elements.
CPE4E elements.
CPE6E elements.
CPE8E elements.
CPE8RE elements.
Linear elastic, Young's modulus 30 × 106, Poisson's ratio 0.3, no piezoelectric coupling, isotropic dielectric constant 1.0 × 10–3.
Boundary conditions:
, 
, 
, 
, 
.
Loading:
Distributed pressure of 1000/area on each face, and equivalent concentrated forces for shear loading, defined such that all three shear stresses are of magnitude –1000.
Distributed charges of 1000/area on each face.
Concentrated charges at each node to negate the distributed charges, except for the distributed charge of 1000/area on the top surface.
Stresses
–1000.
Strains
–1.3333 × 10–5, 
–8.6667 × 10–5.
Electrical fluxes
0, 0, 
–1000.
Electrical potential gradients
0, 0, 
–1.0 × 106.
Displacements
.
Potentials
.
Elements using reduced integration may have additional boundary conditions to those specified above. All elements yield exact solutions.
The *SECTION FILE and *SECTION PRINT output requests are used in some of the input files to output accumulated quantities on the face in the – plane.
C3D4E elements.
C3D6E elements.
C3D8E elements.
C3D10E elements.
C3D15E elements.
C3D20E elements.
C3D20RE elements.
Linear elastic, Young's modulus 30 × 106, Poisson's ratio 0.3, no piezoelectric coupling, isotropic dielectric constant 1.0 × 10–3.
Boundary conditions:
.
Loading:
Distributed pressure of 1000/area on each face.
Distributed charges of 1000/area on each face.
Concentrated charges at each node to negate the distributed charges, except for the distributed charge of 1000/area on the top surface.
Stresses
–1000, 
0.
Strains
–1.3333 × 10–5, 
0.
Electrical fluxes
0, –1000.
Electrical potential gradients
0, –1.0 × 106.
Displacements
= –1.33 × 10–2 along 
1000, 
–1.33 × 10–5
.
Potentials
.
Elements using reduced integration may have additional boundary conditions to those specified above. All elements yield exact solutions.
The *SECTION FILE and *SECTION PRINT output requests are used in some of the input files to output accumulated quantities on the face in the – plane.
CAX3E elements.
CAX4E elements.
CAX6E elements.
CAX8E elements.
CAX8RE elements.