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.
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Max Tension [kN]
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Max Compression [kN]
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Max Displacement [mm]
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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.