Euler Buckling (2D)

Critical load P_cr—
Applied load P—
Load ratio P/P_cr—
Safety factor—
StatusSTABLE
P_cr = π²·E·I / (K·L)². Deflection shape is the true first buckling eigenmode for the selected end condition (half-sine, full-sine, cantilever quarter-cosine, or the fixed-pinned approximation).