Brace Non Slender Column Design
Biaxial Bending
Desing of column between ground floor and first floor. Aassume foundation is at ground floor level. Hence, moments at ground floor level are zero.
- 400mm square column
- Axial Load NEd = 3000kN
- Moments at top My = 110kNm and Mz = 130kNm
- Moments at Bottom are zero
- fck 30N/mm2
- fyk 500N/mm2
- Nominal Cover 25mm
- Floor to Floor height 4000mm
- Depth of the beam supported by the column 500mm
My = 110 kNm
NEd = 3000 kN
Clear height = 4000-500
= 3500mm
Effective length = lo
= factor * l
Factor = 0.85 (concise Eurocode 2, Table 5.1. This may more conservative).
lo = 0.85* 3500
= 2975mm
Slenderness λ = lo/i
i = radios of gyration
= h/√12
λ = lo/( h/√12 )
= 3.46*lo/h
= 3.46*2975/400
= 25.73
Limiting Slenderness λlim
λlim = 20ABC/√n
A = 0.7 if effective creep factor is unknown
B = 1.1 if mechanical reinforcement ratio is unknown
C = 1.7 - rm
= 1.7-Mo1/Mo2
Mo1 = 0 kNm
Mo2 = 130kNm where lMo2l ≥ lMo1l
C = 1.7 - 0/130)
= 1.7
n = NEd / (Ac*fcd)
fcd = fck / 1.5
= (30/1.5)*0.85
= 17
n = 3000*1000 / (400*400*17)
= 17
n = 3000*1000 / (400*400*17)
= 0.94
λlim = 20*0.7*1.1*1.7/√0.94
= 27
λlim > λ hence, column is not slender.
Calculation of design moments
Column has moments in both directions.
First find the critical moment.
Consider My,
Consider My,
Assume there is no moment at ground floor level as foundations are at that level.
MEdy = Max{Mo2, MoEd +M2, Mo1 + 0.5M2}
Mo2y = Max {Mtop, Mbottom} + ei*NEd
= 110 + (2.975/400)*3000 ≥ Max(400/30, 20)*3000
= 110+22.3 ≥ 60
= 132.3kNm > 60kNm
Mo1y = 0
MoEdy = 0.6*Mo2+ 0.4*Mo1 ≥ 0.4*Mo2
= 0.6*132.3 + 0.4*(0) ≥ 0.4*132.3
= 79.4≥ 52.9
M2y = 0 , Column is not slender
MEdy = Max{Mo2, MoEd +M2, Mo1 + 0.5M2}
= Max{132.3, 79.4+0, 0 + 0.5*0}
= 132.3 kNm
Consider Mz,
Assume there is no moment at ground floor level as foundations are at that level.
MEdz = Max{Mo2, MoEd +M2, Mo1 + 0.5M2}
Mo2z = Max {Mtop, Mbottom} + ei*NEd
= 130 + (2.975/400)*3000 ≥ Max(400/30, 20)*3000
= 130+22.3 ≥ 60
= 152.3 kNm > 60 kNm
Mo1z = 0
MoEdz = 0.6*Mo2+ 0.4*Mo1 ≥ 0.4*Mo2
= 0.6*152.3 + 0.4*(0) ≥ 0.4*152.3
= 91.4≥ 60.9
M2z = 0 , Column is not slender
MEdz = Max{Mo2, MoEd +M2, Mo1 + 0.5M2}
= Max{152.3, 91.4+0, 0 + 0.5*0}
= 152.3 kNm
Imperfection needs to be considered only in one direction, which has the most unfavorable effect.
Therefore,
MEdz = 132.3kNm and MEdy = 130kNm
Consider Critical Moment MEdz = 132.3kNm
MEd / [b*(h^2)*fck] = (132.3*10^6) / [400*(400^2)*30]
= 0.07
NEd / (b*h*fck) = (3000*10^6) / (400*400*30
= 0.63
Assume 25mm diameter bars as main reinforcement and 10mm bars as shear links
d2 = 25+10+25/2
= 47.5mm
d2/h = 47.5 / 400
= 0.12
Note: d2/h = 0.15 chart is reffed to find the reinforcement area, but it is more conservative. Interpolation between charts d2/h = 0.10 and d2/h = 0.15 can be used to find more accurate answer.
As*fyk / b*h*fck = 0.3
As = 0.3*400*400*30 / 500
= 2880mm2
Provides six 25mm bars (As Provided 2940mm2)
Six 25mm bars are provided for bending, but colulmn have to be reinforced symmetrically. Therefor total no of base provided for the column are eight.
Further check is not required if
0.5 ≤ ( λy/ λz) ≤ 2.0 For rectangular column
and
0.2 ≥ (ey/heq)/(ez/beq) ≥ 5.0
Here λy and λz are slenderness ratios
λy is equal to λz as beam height is each directions are similar.
therefore λy/λz = 1
Hence, λy/λz < 2 and > 0.5 OK
ey/heq = (MEdz / NEd) / heq
ez/beq = (MEdy / NEd) / beq
(ey/heq)/(ez/beq) = MEdz / MEdy Here h=b=heq=beq, column is square
MEdz = 130 kNm
MEdy = 132.3 kNm
(ey/heq)/(ez/beq) = 130/132.3
= 0.98 > 0.2 and < 5
Therefore, biaxial check is required.
(MEdz / MRdz)^a + (MEdy / MRdy)^a ≤ 1
MEdz = 130kNm
MEdy =132.3kNm
MEdy = 132.3 kNm
(ey/heq)/(ez/beq) = 130/132.3
= 0.98 > 0.2 and < 5
Therefore, biaxial check is required.
(MEdz / MRdz)^a + (MEdy / MRdy)^a ≤ 1
MEdz = 130kNm
MEdy =132.3kNm
MRdz and MRdy are the moment resistance in respective direction, corresponding to an axial load NEd.
For symetric reinforcement section
MRdz = MRdy
As Provided = 2940mm2
As*fyk / b*h*fck = 2940*500/(400*400*30)
= 0.31
= 0.31
NEd / (b*h*fck) = 0.63
From the chart d2/h =0.15
From the chart d2/h =0.15
MEd / [b*(h^2)*fck] = 0.075
NEd = 3000kN
NRd = Ac*fcd + As*fyd
NRd = 400*400*(0.85*30/1.5) + 3920*(500/1.15)
= 4424kN
NEd / NRd = 3000/4424
= 0.68
By interpolating
a = 1.48
(MEdz / MRdz)^a + (MEdy / MRdy)^a = (130 / 144)^1.48 + (132 / 144)^1.48
MEd = 0.098*400*400*400*30
= 144kNm
a = an exponent
a = 1.0 for NEd / NRd = 0.1
a = 1.5 for NEd / NRd = 0.7
= 144kNm
a = an exponent
a = 1.0 for NEd / NRd = 0.1
a = 1.5 for NEd / NRd = 0.7
NEd = 3000kN
NRd = Ac*fcd + As*fyd
NRd = 400*400*(0.85*30/1.5) + 3920*(500/1.15)
= 4424kN
NEd / NRd = 3000/4424
= 0.68
By interpolating
a = 1.48
(MEdz / MRdz)^a + (MEdy / MRdy)^a = (130 / 144)^1.48 + (132 / 144)^1.48
= 1.74 > 1
Hence, Check for biaxial bending is not ok
Therefore, increase the noumner of bars to 12 (In this design, the reinforcement along the two sides have only taken to account for this design and effect of the other reinforcement bars at in opposit direction have not been considered).
Therefore no of reinforcements, which are effctive for moment resistance are eight (3920mm2) and twelve are effctive for axial capasity (5880mm2).
Hence, Check for biaxial bending is not ok
Therefore, increase the noumner of bars to 12 (In this design, the reinforcement along the two sides have only taken to account for this design and effect of the other reinforcement bars at in opposit direction have not been considered).
Therefore no of reinforcements, which are effctive for moment resistance are eight (3920mm2) and twelve are effctive for axial capasity (5880mm2).
As*fyk / b*h*fck = 3920*500/(400*400*30)
= 0.41
= 0.41
NEd / (b*h*fck) = 0.63
From the chart d2/h =0.15
From the chart d2/h =0.15
MEd / [b*(h^2)*fck] = 0.105
NEd = 3000kN
NRd = Ac*fcd + As*fyd
NRd = 400*400*(0.85*30/1.5) + 3920*(500/1.15)
= 4850kN
NEd / NRd = 3000/4850
= 0.62
By interpolating
a = 1.43
(MEdz / MRdz)^a + (MEdy / MRdy)^a = (130 / 202 )^1.43 + (132 / 202 )^1.43
MEd = 0.105*400*400*400*30
= 202 kNm
a = an exponent
a = 1.0 for NEd / NRd = 0.1
a = 1.5 for NEd / NRd = 0.7
= 202 kNm
a = an exponent
a = 1.0 for NEd / NRd = 0.1
a = 1.5 for NEd / NRd = 0.7
NEd = 3000kN
NRd = Ac*fcd + As*fyd
NRd = 400*400*(0.85*30/1.5) + 3920*(500/1.15)
= 4850kN
NEd / NRd = 3000/4850
= 0.62
By interpolating
a = 1.43
(MEdz / MRdz)^a + (MEdy / MRdy)^a = (130 / 202 )^1.43 + (132 / 202 )^1.43
= 1 (nearly equals to one)
Hence, Provided reinforcemts are ok.
Hence, Provided reinforcemts are ok.
Note :
This column is design for biaxial bending. This mathod is like trial and error method. Becouse, this has to be done untill (MEdz / MRdz)^a + (MEdy / MRdy)^a < 1, but Manual for the design of concrete building structures to Eurocode 2 and the book, Reinforced concrete design to Eurocode 2 written by Bill Mosley, John Bungey and Ray Hulse have suggested the old method, which is in BS 8110.
Old method is more straight forward than this method, because once we have find the biaxial moment then we can find the reinforcement area easily.
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ReplyDeleteHi, It is great. I'm happy to cooperate if there is any thing that I could do.
ReplyDeletethanks, it is really helpful :)
ReplyDeletehi, i am new to design, May i know why the Ned becomes 3000kN? Thanks a lot
ReplyDeleteHi
ReplyDeleteVery sorry for late response
It is a data.
It is in the top of the page
Please visit my website where you may download free software for design of columns subjected to biaxial bending to BS8110 and ACI318
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in the last step CALCULATION OF nrd
ReplyDeleteyou take fcd*0.85/1.5 and fyd/1.15 ??
how it is taken? any code reference??
for fcd - Cl 3.1.6 of EC2
ReplyDeletefor fyt - figure 3.8 of EC2
its been so helpful. thanks
ReplyDelete