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DWG TITLEPORTFOLIO BLUEPRINT
DRAWN BYDINESH KUMAR
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REVISIONA.02
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Structural Mechanics

Euler Buckling Simulator

Examine elastic column buckling limits under compressive loads. Toggle boundary conditions to see physical mode shapes, slenderness effects, and load capacities.

Class
Long Column
λ = 400
Critical Load
24.2 kN
Elastic threshold
Output
CSV
Export ready

Parameters

Boundary Conditions
Length Sweep Sweep

Structural Equations

Euler Critical Buckling Load (Pcr)
Pcr = (π² * E * I) / (K * L)²
Moment of Inertia (Circular Section)
I = (π * d⁴) / 64
Slenderness Ratio (λ)
λ = Le / r where r = sqrt(I/A)

Column diameter: 50 mm (Area = 19.63 cm²).

Effective Length Le = K * L = 5.00 m (Boundary factor K = 1).

Buckling Response & Support Model

Pcr = 24.2 kNL = 5.0 md = 50 mmK = 1.0 (Pinned-Pinned)
Critical Load (Pcr)
24.2kN
Slenderness Ratio
400.0
Effective Length (Le)
5.00m
Moment of Inertia (I)
30.68cm⁴

Critical Load (Pcr) vs Column Length

Buckling Stability Profile

Length L (m)Slenderness RatioCritical Load (kN)
1.0080.0605.6
1.50120.0269.1
2.00160.0151.4
2.50200.096.9
3.00240.067.3
3.50280.049.4
4.00320.037.9
4.50360.029.9
5.00400.024.2
5.50440.020.0
6.00480.016.8
6.50520.014.3
7.00560.012.4
7.50600.010.8
8.00640.09.5
8.50680.08.4
9.00720.07.5