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COLUMN BUCKLING (EULER & JOHNSON)

SLENDERNESS RATIO, END-CONDITION K, EULER-JOHNSON TRANSITION

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WHAT IT COMPUTES

Long compression members fail by buckling rather than yielding. Euler's formula P_cr = π²EI / (KL)² governs slender columns where buckling stress stays below yield. K is the end-condition factor: 0.5 (fixed-fixed), 0.7 (fixed-pinned), 1.0 (pinned-pinned), 2.0 (fixed-free). For shorter columns the actual failure stress curves below Euler's prediction; the Johnson formula handles this transition region using yield strength. The crossover slenderness is (KL/r)_t = sqrt(2π²E/Sy).

KEY EQUATIONS

References & StandardsAISC 360 Ch. E, Shigley 4.11, Norton 4.16

WHEN TO USE THIS MODULE

Apply column analysis to any compression member: pneumatic-cylinder rod extended fully (treat as fixed-pinned with K=0.7), forklift mast, screw-jack lead screw, structural strut, scaffolding leg. Compute slenderness ratio KL/r first; if above (KL/r)_t use Euler, otherwise use Johnson. Apply factor of safety 2-4 depending on dynamic loading and uncertainty in end conditions.

RELATED MODULES

SECTIONS

Area, centroid, moment of inertia, section modulus, radius of gyration

STRESS

Principal stresses, max shear, von Mises, Tresca yield

SHAFTS

Torsional stress, twist angle, Rayleigh critical speed, keyway sizing

FATIGUE

Mean-stress diagrams, endurance limit modifiers, infinite life

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