Design for bending for flanged sections (concrete beam: EC2)

Tekla Structural Designer
Modified: 10 Nov 2022
2025
Tekla Structural Designer

Design for bending for flanged sections (concrete beam: EC2)

IF hf < 0.1*d THEN treat the beam as rectangular.

hf = MIN(hf,side1, hf,side2)

where

hf,sidei = the depth of the slab on side " i" of the beam

Calculate the value of K from;

K = MEd/(fck*beff*d2)

Calculate the lever arm, z from;

z = MIN(0.5*d*[1 + (1 - 2*K/(η*αccC))0.5], 0.95*d)

Calculate the depth of the rectangular stress block, λ*x from;

λ*x = 2*(d-z)

   

IF λ*x ≤ h f THEN the rectangular compression block is wholly in the depth of the flange and the section can be designed as a rectangular section by setting bw = beff.

   

IF λ*x > h f THEN the rectangular compression block extends into the rib of the flanged section and the following design method is to be used.

The design bending strength of the flange, Mf is given by;

Mf = fcd*hf*(beff-bw)*(d-0.5*h f)

The area of reinforcement required to provide this bending strength, Asf,reqd is given by;

Asf,reqd = Mf/(fyd*(d-0.5*hf))

The remaining design moment, (MEd-Mf) is then taken by the rectangular beam section.

Calculate the value of K from;

K = (MEd-Mf)/(fck*bw*d2)

Then calculate the limiting value of K, known as K' from;

K' = (2*η*αccC)*(1 - λ*(δ - k1)/(2*k2))*( λ*(δ - k1)/(2*k2)) for fck ≤ 50 N/mm2

K' = (2*η*αccC)*(1 - λ*(δ - k3)/(2*k4))*( λ*(δ - k3)/(2*k4)) for fck > 50 N/mm2

   

IF K ≤ K' THEN compression reinforcement is not required.

Calculate the lever arm, z from;

z = MIN(0.5*d*[1 + (1 - 2*K/(η*αccC))0.5], 0.95*d)

The area of tension reinforcement required is then given by;

Asr,reqd = (MEd-Mf)/(fyd*z)

The total area of tension reinforcement required, Ast,reqd is then given by;

Ast,reqd = Asf,reqd+Asr,reqd

The depth to the neutral axis, xu is given by;

xu = 2*(d-z)/λ

   

IF K > K' THEN compression reinforcement is required.

Calculate the depth to the neutral axis from;

xu = d*(δ-k1)/k2 for fck ≤ 50 N/mm2

xu = d*(δ-k3)/k4 for fck > 50 N/mm2

   

Calculate the stress in the reinforcement from;

fsc = MAX(Escu3*(1-(d2/xu), fyd)

where

d2 = the distance from the extreme fibre in compression to the c of g of the compression reinforcement

Calculate the limiting bending strength, M' from;

M' =K'*fck*bw*d2

Calculate the lever arm from;

z = 0.5*d*[1 + (1 - 2*K'/(η*αccC))0.5]

The area of compression reinforcement required, As2,reqd is given by;

As2,reqd = (MEd-Mf-M')/(fsc*(d-d2))

The area of tension reinforcement required, Asr,reqd is given by;

Asr,reqd = M'/(fyd*z) + As2,reqd*fsc/fyd

The total area of tension reinforcement required, Ast,reqd is then given by;

Ast,reqd = Asf,reqd+Asr,reqd

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