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001027
2023-12-29

Расчетное значение критической потери устойчивости при изгибе сжатого стержня вдоль второстепенной оси, FcEy.

Critical Buckling Design Value for Compression Member in Minor Axis, FcEy

FcEy = FcE2 = 0.822 · Emin'le2d22
FcEy = FcE2 = 0.822 · 510,000 psi36.0 in1.5 in2
FcEy = FcE2 = 728 psi

FcEy

Critical buckling design value for the compression member in the minor axis, psi

Emin'

= Emin ⋅ CM ⋅ CT ⋅ Ci = 510,000 psi

le2

Effective length = 36.0 in

d2

Member thickness = 1.5 in
;