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ONESTEEL duragal sections

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PART 5<br />

MEMBERS SUBECT TO AXIAL<br />

COMPRESSION<br />

D5.1 SCOPE<br />

The following tables give values of design axial compression capacity for various effective lengths and<br />

have been determined using Section 6 of AS 4100.<br />

All loads are assumed to be applied through the centroid of the section and the column capacity is assumed<br />

to be associated with flexural buckling about either the x- or y-axis.<br />

D5.2 DESIGN CAPACITY FOR MEMBERS SUBJECT TO<br />

AXIAL COMPRESSION<br />

Values of the design capacity for axial compression (φN c ) for buckling about both principal axes, based on<br />

the appropriate effective length (L e ), are given in Tables D5.2-1 to D5.2-4.<br />

The tables in this section have been grouped into two series for rectangular hollow <strong>sections</strong>:<br />

• the (A) series (e.g. Table D5.2-1(1)(A)) for the member buckling about the x-axis, and<br />

• the (B) series (e.g. Table D5.2-1(1)(B)) for the member buckling about the y-axis.<br />

The (A) series tables are immediately followed by the (B) series tables.<br />

D5.3 METHOD<br />

The design axial compression member capacity is obtained from Clauses 6.3 of AS 4100 and is given by:<br />

φN c = φ α c N s<br />

≤ φN s<br />

where φ = 0.9 (Table 3.4 of AS 4100)<br />

φN s = φ k f A n f y (see Section D3.2.2 and Tables D3.1-1 to D3.1-4)<br />

k f = A e /A g (see Section D1.2.3.3 and Clause 6.2.2 of AS 4100)<br />

A n = net section area<br />

= A g<br />

= gross cross-sectional area (assumed no penetrations or holes)<br />

f y = yield stress used in design<br />

α c = member slenderness reduction factor<br />

DuraGal DESIGN CAPACITY TABLES<br />

DCTDHS/06<br />

D5-2 for STRUCTURAL STEEL HOLLOW SECTIONS MARCH 2002

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