steel design aisc

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Compression Members Local Stability

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Page 1: Steel design AISC

Compression Members

Local Stability

Page 2: Steel design AISC

• It is permissible to use a cross-sectional shape that does not satisfy the width-thickness ratio requirements, but such a member may not be permitted to carry as large a load as one that does satisfy the requirements. In other words, the strength could be reduced because of local buckling.

Page 3: Steel design AISC

• The reduction factor Q is the product of two factors: Qs for unstiffened elements and Qa for stiffened elements. Q = (Qs)(Qa)

• For cross sections composed of only unstiffened slender elements, Q = Qs(Qa = 1.0).

• For cross sections composed of only stiffened slender elements, Q = Qa(Qs = 1.0).

• For cross sections composed of both stiffened and unstiffened slender elements, Q = (Qs)(Qa).

Page 4: Steel design AISC
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• Example: Determine the axial compressive strength of an HSS 200 x 100 x 3 with an effective length of 4600mm with respect to each principal axis. Use Fy = 315 Mpa.

Page 7: Steel design AISC

Design

• Example: Select an I-Shape steel with an overall depth of 500mm that can resist a service dead load of 445KN and a service live load of 1335KN. The effective length KL is 8000mm and Fy = 345Mpa.

Page 8: Steel design AISC

More on Effective Length

• Example: An I 300 x 250 x 16(tf) x 9(tw) steel 7500mm long is pinned at both ends and braced in the weak direction at the third point as shown in the drawing. Fy = 345Mpa. Determine the available compressive strength.

13’ = 4m

2500mm

2500mm

2500mm

y-direction

7500mm

x-direction

Page 9: Steel design AISC

Torsional and Flexural-Torsional Buckling

• When an axially loaded compression member becomes unstable overall (that is, not locally unstable), it can buckle in one of three ways:

1. Flexural Buckling: It is a deflection caused by bending, or flexure, about the axis corresponding to the largest slenderness ratio. This usually the minor principal axis – the one with the smallest radius of gyration. Compression members with any type of cross-sectional configuration can fail in this way.

2. Torsional Buckling: This type of failure is caused by twisting about the longitudinal axis of the member. It can occur only with doubly symmetrical cross sections with very sender cross-sectional elements.

3. Flexural-Torsional Buckling: This type of failure is caused by a combination of flexural bucking and torsional buckling. The member bends and twists simultaneously. This type of failure can occur only with unsymmetrical cross sections, both those with one axis of symmetry such as channels, structural tees, double-angle shapes, and equal-leg single angles, and those with no axis of symmetry such as unequal-leg single angles.

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• Example: Compute the compressive strength of a structural tee T 320(d)x330(bf)x18(tw)x30(tf). The effective length with respect to the x-axis is 7800mm, the effective length with respect to the y-axis is 6100mm, and the effective length with respect to the z-axis is 6100mm. Fy = 345Mpa.

Page 13: Steel design AISC

End of Compression Members