2D Truss Analyzer Back EN | ZH
Structural FEM

2D Truss Analyzer

Direct Stiffness Method (FEM) solver for planar trusses. Members color-coded by axial force — tension in red, compression in blue.

Truss Configuration
Preset Geometry
Young's Modulus E 200 GPa
Cross-section Area A 10.0 cm²
Nodal Loads
Positive = right / up. Edit and press Enter.
Max Tension [kN]
Max Compression [kN]
Max Displacement [mm]
Nodes / Members
Tension (+)
Compression (−)
Zero force
Support node

Theory (Direct Stiffness Method)

Assemble element stiffness matrices into the global system and solve:

$$[K]\{u\}=\{F\}$$

Member axial force from nodal displacements:

$$f = \frac{EA}{L}\bigl[(u_j-u_i)\cos\theta + (v_j-v_i)\sin\theta\bigr]$$

Element stiffness: $k = EA/L$, transformed to global DOFs via rotation matrix.

CAE Note: Identical formulation to ANSYS LINK180 and Abaqus T2D2 truss elements. Use this tool for preliminary member sizing before building a full FEM model, or to verify hand calculations in structural design coursework.