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Course · lesson 3 of 5

Rafters and columns as beam-columns

The members of the lesson 1 frame under portal actions to EN 1993-1-1: where the moments are, the sway check αcr and the imperfections, the buckling lengths in and out of the frame’s plane, purlins and fly braces, uplift, and serviceability, with the STATIX steel member calculator on its Eurocode 3 route.

1. Learning outcomes

After this lesson you can:

  • read portal frame actions and choose the check sections;
  • check αcr and add the sway imperfection to the gravity case;
  • set in-plane and out-of-plane lengths for a column and a rafter, with purlins, girts and fly braces;
  • check the rafter under gravity and under uplift with (6.61) and (6.62);
  • check eaves sway and apex deflection against agreed limits.

2. Before you start

3. Portal actions

eavesnear the apexgravity: hogging at the eaves, sagging near the apex
Portal actions under gravity. The rafter carries a large moment and a small axial force; the column carries the axial force and the eaves moment, which falls to zero at a pinned base. The free steel member calculator checks one section at a time with the actions you bring from a frame analysis; STATIX 3D does that analysis in the model.
inner flange in compressionuplift: the moments reverse along the rafter
Portal actions under uplift. With the light roof lifted by wind (1.0 G + 1.5 W), the moments reverse: along the middle of the rafter the inner (bottom) flange goes into compression, where gravity never put it, and the bases go into tension.
haunch tip: the plain rafter startscolumn below the haunchnear the apex
Where to check. The column just below the haunch, the rafter at the haunch tip where the deeper section ends, and the rafter near the apex. Inside the haunch the section is deeper; the haunch and its connection are lesson 4.

4. Sway and imperfections

Hδαcr = (HEd/VEd) (h/δH,Ed)≥ 10: first-order analysis is enough (5.2.1(3))
Sway and αcr (EN 1993-1-1 5.2.1). A portal is unbraced in its own plane: under a horizontal force it sways, and the vertical loads acting on the sway add moment. For portal frames with shallow roofs, 5.2.1(4)B estimates the elastic critical factor αcr from the sway δ under the horizontal forces; if αcr ≥ 10, first-order moments are enough; between 3 and 10 they are amplified (5.2.2(5)); below 3, a second-order analysis is needed.
sway imperfection φ = φ0 αh αmφ0 = 1/200; αh = 2/√h (2/3 to 1); αm = √[0.5(1 + 1/m)]equivalent forces φ N at the column tops (5.3.2(7))
Imperfections (5.3.2). No frame is built plumb. EN 1993-1-1 represents the out-of-plumb by a sway imperfection φ, applied as equivalent horizontal forces φ NEd at the column tops. They may be left out where the horizontal loads are large (HEd ≥ 0.15 VEd, 5.3.2(4)), as in the wind cases, but not in the gravity case.
αcr = (HEd / VEd) (h / δH,Ed) (5.2.1(4)B; shallow roofs, small rafter axial force) αcr ≥ 10: first-order; 3 ≤ αcr < 10: amplify the sway effects by 1/(1 − 1/αcr) (5.2.2(5)); < 3: second order φ = φ0 αh αm; equivalent horizontal force at a column top: φ NEd (5.3.2(3), (7))

5. Buckling lengths and restraint

column, in planethe storey height; sway and imperfections in the analysiscolumn, out of planebetween girts with fly braces, or the full heightrafter, in planeeaves to apex (a safe practice value)rafter, out of planethe compression flange’s restraint spacing
Buckling lengths as this course uses them. When the sway effects and the imperfections are in the global analysis (5.2.2(3) b), the members are checked with their own system lengths. Out of plane, the length is the distance between real restraints of the compression flange.
purlins: hold the top flangefly braces (red): hold the inner flangeunder uplift the inner flange needs them
Restraint. Purlins hold the rafter’s top flange at their spacing; fly braces from a purlin (or girt) to the inner flange restrain the bottom flange where they are fitted. Which flange is in compression decides which spacing is the lateral-torsional buckling length.
gravityupliftnear the eaves: bottommid-rafter: bottomred: the flange in compression that purlins do not hold
Which flange is in compression. Under gravity, the inner (bottom) flange is in compression near the eaves and the top flange near the apex; under uplift, the bottom flange along the middle of the rafter. The purlins only ever hold the top flange.

6. The member checks

6.2.9the section under N and M6.3.1flexural buckling about y and z6.3.2lateral-torsional buckling, Mb,Rd6.3.3(6.61), (6.62) with the Annex B factorsCm = 0.9sway frame; Frame unbraced sets it
The member checks are those of Steel Design 1 (Eurocode) lesson 4. For a member of a sway frame Table B.3 takes Cmy = Cmz = 0.9; on the steel member calculator, Frame “unbraced” sets this unless you type Cm.

What the steel member calculator’s Eurocode 3 route uses here: the checks of Steel Design 1 (Eurocode) lesson 4, run by the calculator’s steel member engine (6.2.9, 6.3.1, 6.3.2, and 6.3.3 with the Annex B factors), γM0 = γM1 = 1.0, and Frame “unbraced” giving Cmy = Cmz = 0.9 with a note that the moments and lengths must be those of a sway frame. It does not analyse the frame: you bring N, M and V for each section. It also lists flange-induced buckling of the web and the torsional buckling of the member.

7. Serviceability

apex deflectioneaves swayservice loads; limits agreed with the client (7.2)
Serviceability (EN 1993-1-1 7.2). Check the sideways movement of the eaves under wind and the vertical movement of the apex under the roof loads, with characteristic combinations. EN 1993-1-1 leaves the limits to the national annex and the client; agree them with the client and the cladding supplier.

8. In STATIX

frameanalysis (3D)αcr, φ5.2, 5.3sectionN, M, Vmembercalculator
The route: analyse the frame (STATIX 3D does it in the model; this lesson gives the actions from a simple elastic analysis), check αcr and the imperfections, then check each section in the steel member calculator on its Eurocode 3 route with the lengths that match the restraints and Frame set to unbraced.

9. Example A: the frame under gravity

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10. Example B: the frame under uplift

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11. Do it in STATIX

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12. Common mistakes

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13. Exercises

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14. Self-check quiz

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15. Lesson 3 on one page

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Next: Lesson 4, the eaves haunch connectionBolt rows as T-stubs, Mj,Rd, the compression zone, the column web panel, welds and the reversed moment.
Go to lesson 4

A worked example for learning, not a design. Check every value against the current code, your national annex and your own project, and have the design checked and signed by a registered professional engineer.

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