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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