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Page 1: Bracing a

Sheet . . . . . . .of . . . . .PROJECT : Job No :SUBJECT : Revision :Calc by : Date : 02-jan-2015 Checked : Date :

Code check single angle to AISC 360-10 LRFD

Design loads kN kN-m

Axial load (Pr) = 163,17 Moment x-x (Mrx) = 0,00

(short leg) (Vrx) = 0,00 Moment y-y (Mry) = 0,00

(long leg) (Vry) = 0,00

Moments resolved about principal axes (F10). Theta = 45,00

Mw-w = 0,00 Mz-z = 0,00

Effective lengths

Lb (F10) = 4742 E5.(a) KL/rx' = 4742

Section data

150x150x15 RSA Fy =355,0 MPa

D = 150,00 B = 150,00 tw = 15,00 Area = 4.320,000 mm2

Points 1 2

Sx 84.636,872 213.380,282 mm3

Sy 213.380,282 84.636,872 mm3

Iw = 14400000,000 Iz = 3750000,000 mm4

rw = 57,74 rz = 29,46 mm

Lw/rw = 82,13 Lz/rz = 0,00

Points 1 2 3

Sw 135.764,464 -135.764,540 mm3

Sz 82.932,406 82.932,148 -61.628,573mm3

Section available stresses

Point 1 Point 2 Point 3

Fa(c) = 0,1 0,1 0,1

Fa(t) = 0,1 0,1 0,1

Fbw = 351,5 351,5 351,5

Fbz = 356,1 356,1 479,3

Code check results

Cb = 1

(H2-1) point 1 0,13 + 0,00 + 0,00 = 0,13

point 2 0,13 + 0,00 + 0,00 = 0,13

point 3 0,13 + 0,00 + 0,00 = 0,13

Shear

On short leg Vr.x /Vc.x = 0,00

On long leg Vr.y /Vc.y = 0,00

Section O.K. use 150x150x15 RSA

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