Specimen: I-Beam Cantilever · FEA Reference
ASTM-A36E = 200 GPa
X: 0.000 m
Y: +0.250 m
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+
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L = 2.40 mP = 18.5 kNδ = 14.2 mmTensile Stress (σ > 0)Compressive Stress (σ < 0)Neutral Axis
Tensile Compressive
Moment Eq.M(x) = -P(L-x)
Peak Stressσ_max = 142 MPa
Safety Factorn = 1.76 (Safe)
Curvatureκ = M / EI
Unified Structural Principles

Engineering in the Real World

The exact same principles of solid mechanics dictate how structures bear load—whether calculating wing spar flex in high-speed flight, deck deflection across a suspension bridge, or torque transfer through a drive axle.

AERO-01Aircraft Wings
Bending & Shear Flow
CIVIL-04Bridge Trusses
Axial Tension/Compression
AUTO-02Automotive Chassis
Torsional Rigidity
MECH-09Turbine Shafts
Combined Torsion & Bending
Grounded in Hibbeler, Gere & Goodno Mechanics of Materials