Frame eigenvalue problem

Image of truss

Objective

To verify the truss element when used with skew coordinate systems.

Problem description

The truss structure is shown in figure below. Numerical values for this problem are: E=2e11, L=5.0, A=0.0001, b=h=0.5, P=1000 (units: N, m).

Finite element model

The truss structure is modeled with 2-node truss elements. The structure is inclined in the global coordinate system so it is effective to employ skew coordinate systems.

Image of the model 

Solution

The displacement of the point of load application in the direction of the cantilever is:

Image of the displacement of the point of load application in the direction of the cantilever 

This displacement is calculated and compared to that calculated by FEEA:

The displacement of the point of load application in the direction of the cantilever
Displacement FEEA Theory
Node 221.125E-31.125E-3

The internal forces of some elements also are shown below:

The internal forces of some elements
Internal Force Nodes FEEA Theory
Element 11,2-10000.00-10000.00
Element 22,3-9000.00-9000.00
Element 1112,139000.009000.00
Element 2112,21414.211414.21

Conclusion

The results obtained with FEEA SDK show that it handles efficiently multiple coordinate systems, and nodes assigned skew coordinate systems.