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 x–y 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 x–y 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 × 10–5z.
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 x–y plane.
CAX3E elements.
CAX4E elements.
CAX6E elements.
CAX8E elements.
CAX8RE elements.