CQPSTS

Bulk Data Entry Plane stress quadrilateral element connection. Defines a plane stress quadrilateral element in the x-z or x-y plane.

Format

(1) (2) (3) (4) (5) (6) (7) (8) (9) (10)
CQPSTS EID PID G1 G2 G3 G4 G5 G6  
  G7 G8 Theta            

Example

(1) (2) (3) (4) (5) (6) (7) (8) (9) (10)
CQPSTS 111 2 31 74 75 32 51 52  
  53 85 15.0            

Definitions

Field Contents SI Unit Example
EID Unique element identification number.

No default (Integer > 0)

  
PID A PPLANE entry identification number.

Default = EID (Integer > 0)

  
G1, G2, G3, G4 Identification numbers of connected corner grid points.

These fields are mandatory.

No default (Integers > 0, all unique)

  
G5, G6, G7, G8 Identification numbers of connected edge grid points.

No default (Integers > 0 or blank)

  
Theta Material orientation angle in degrees.

Default = 0.0 (Real)

  

Comments

  1. Element identification numbers must be unique with respect to all other element identification numbers.
  2. The grid ordering of G1 through G8 is defined as:


    Figure 1.
  3. The continuation is optional.
  4. The definition of the elemental coordinate system and material orientation angle theta is the same as defined for CQUAD4 and CQUAD8, depending on the number of nodes in the CQPSTS elements.
  5. Plane stress analysis defined in the x-y plane is supported, that is, the axis labels of “z” can be replaced by “y”. The out-of-plane normal direction defined by the corner node sequence with the right hand rule should point to the z direction if the element is in the x-y plane, or the -y direction if in the x-z plane.
  6. A concentrated load (for example, a load specified by a FORCE entry) at a grid Gi of this element is defined to distribute along the thickness, T, of the element. For example, to apply a load of 200 N/m to a node Gi with the element thickness being 0.05 m, the amount to be specified on the load entry should be (200N/m) * 0.05m = 10N.

    The default thickness of 1.0 is used if T is not specified on the PPLANE entry.

  7. Plane stress elements are supported in:
    • Linear static analysis
    • Nonlinear Static analysis (Small and large displacement)
    • Linear Transient Analysis
    • Frequency Response Analysis
    • Real and Complex Eigenvalue Analysis
    These elements are currently not supported in:
    • Inertia Relief analysis
    • Buckling analysis
    • Heat transfer analysis
    • Optimization