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Stress Increment in Soil under a Pad Foundation

When foundations are constructed, they increase the net pressure in the soil. The knowledge of this stress increment is very important for estimating the settlement of foundations, and for the evaluation of lateral pressure on adjacent structures.

Boussinesq in 1883 solved the problem of stresses produced at any point in a homogeneous, elastic, and isotropic medium as the result of a point load applied on the surface of an infinitely large half-space. This has been extended into solving most of the problems of stresses that foundations impose on soils and for different types of loading, despite the fact that soils are practically neither homogeneous nor elastic.

In this example, it is required to obtain the stress that a soil mass experiences at a depth of 3m under the pad foundation shown below.

Boussinesq%2Bproblem%2Bquestion

The increment in the stress at any point below a pad foundation can be obtained by following the relationship below.

Boussinesq%2BEquation

For example, let us consider the plan of a pad footing shown below. The loaded area can be divided into four rectangles A, B, C, and D, as shown. It is desired to determine the stress at a point below point 1 at depth z. Note that this point is very common to all four rectangles. The increment in stress at a depth z below point 1 due to each rectangular area can be calculated using the equation above.

Division%2Bof%2Bpad%2Bfooting%2Binto%2Brectangles

The total stress increase caused by the entire loaded area is given by equation (2) below;

∆σz = q [I3(A) + I3(B) + I3(C) + I3(D)] ———- (2)

At the centre of a pad footing, this is given by;

∆σz = q I4   ————– (3)

Where;

I4

For the increment in stress at the centre of a rectangular footing, we can obtain the value of I4 from the Table below (derived from the relationship above);

Table%2Bof%2BI4

Therefore, for the example under consideration;
The service pressure (q) = P/A = (1350 kN) / (1.5m × 1.5m) = 600 kN/m2

b = B/2 = 1.5/2 = 0.75m
m1 = L/B = 1.5m/1.5m = 1.0
n1 = z/b = 3m/0.75m = 4.0

Reading from the table above;
I4 = 0.108

∆σz = q I4
∆σz = 600 × 0.108 = 64.8 kN/m2

Therefore, apart from the overburden pressure (geostatic stress), the stress at a depth of 3m under the pad foundation increased by 64.8 kN/m2 due to the foundation load.

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99.99% of people will be clueless about this puzzle….

The values given for the following triangles were obtained using a consistent relationship. I really do not expect a lot of people to be able figure it out….

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Design of Cantilever Retaining Wall Supporting Lateritic Earth Fill

Cohesive soil profiles due to their nature are partially self supporting up to an extent called the critical depth (the critical depth is given by 2Zo, kindly see figure above). As a result, such soils would not exert much pressure on a retaining wall as a granular material would (especially considering active earth pressure). Tropical laterites (especially those found in Nigeria) usually possess angle of internal friction and some cohesion. Their usage for construction purposes is also widespread.

The walls retaining such soils are subjected to active and passive pressure. In this example, we are going to consider active pressure only (all passive pressure neglected), but note that passive pressure could be more critical and hence govern the design (I recommend you read standard geotechnical engineering textbooks for more knowledge on this subject).

Worked Example

The cantilever retaining wall shown below is backfilled with tropical lateritic earthfill, having a unit weight, ρ, of 18 kN/m3, a cohesion C of 8 kN/m3 and an internal angle of friction, φ, of 26°. The allowable bearing pressure of the soil is 150 kNm/2, the coefficient of friction is 0.5, and the unit weight of reinforced concrete is 24 kN/m3. Water level is at a great depth and adequate drainage is provided at the back of the wall.

Retaining%2Bwall%2Bproblem%2Bquestion

We are to;
1. Determine the factors of safety against sliding and overturning for the active pressure.
2. Calculate ground bearing pressures.
3. Design the wall and base reinforcement assuming fcu = 30 N/mm2, fy = 460 N/mm2 and the cover to reinforcement in the wall and base are, respectively, 40 mm and 50 mm.

Geotechnical Design

Wall Pressure Calculations

Retaining wall with lateritic earth fill

Coefficient of active pressure KA
Using Rankine’s theory
KA = (1 – sinφ) / (1 + sinφ);
KA = (1 – sin 26°) / (1 + sin 26°) = 0.39046;

Pressure at the top of wall = 2C√KA = 2 × 8 × √0.39046 = 9.998 kN/m2
Z0 = 2 C/γ√KA = (2 × 8)/(18 × √0.39046) = 1.423m

Pressure at the bottom of retaining wall = H.γ.KA – 2C√KA = (5.5 × 18 × 0.39046) – (2 × 8 × √0.39046) = 32.408 kN/m2

Earth%2BPressure%2BDiagram

Resistance to Sliding

Consider the forces acting on a 1 m length of wall. Horizontal force on wall due to backfill, PA, is;
PA = 0.5 × 32.408 × 4.077 = 66.063 kN/m

Weight of wall (Ww) = 0.35 × 5.1 × 24 = 42.84 kN/m
Weight of base (Wb) = 0.4 × 4 × 24 = 38.4 kN/m
Weight of soil (Ws) = 2.85 × 5.1 × 18 = 261.63 kN/m
Total vertical force (Wt) = 324.87 kN/m

Friction force, FF, is
FF = μWt = 0.5 × 324.87 = 171.435 kN/m

Neglecting all passive pressure force (FP) = 0.
Hence factor of safety against sliding is;
F.O.S = FF/PA = 171.435/66.063 = 2.595
The factor of safety 2.595 > 1.5. Therefore the wall is very safe from sliding.

Resistance to Overturning

Taking moments about the toe, sum of overturning moments (MO) is;
MO = (66.063 kN/m) × (4.077/3) = 89.779 kN.m

Sum of Restoring Moment MR;
MR = (Ww × 0.975m) + (Wb × 2m) + (Ws × 2.575m)
MR = (42.84 × 0.975m) + (38.4 × 2m) + (261.63 × 2.575m) = 792.266 kNm

F.O.S = MR / MO = 792.266/89.779 = 8.824
The factor of safety 8.824 > 2.0. Therefore the wall is very safe from overturning.

Bearing Capacity Check

Bending moment about the centre line of the base;
M = [66.064 × (4.077/3)] + (Ww × 1.025m) – (Ws × 1m)
M = [66.064 × (4.077/3)] + (42.84 × 1.025m) – (261.63 × 0.575m) = -16.745 kNm

Total vertical load = 324.87 kN

The eccentricity (e) = M/N = (16.745/324.87) = 0.0515m

Let us check D/6 = 4/6 = 0.666
Since e < D/6, there is no tension in the base

The maximum pressure in the base;
qmax = P/B (1 + 6e/B) = 324.87/4 [1 + (6 × 0.0515)/(4)] = 87.491 KN/m2
87.491 KN/m2 < 175 KN/m2

Therefore, the bearing capacity check is satisfied.

Structural Design

Design of the Wall

Conservatively taking the moment at the base of the wall due to the active force;
M = [66.064 × (4.077/3)] = 89.781 kN.m
At ultimate limit state M = 1.4 × 89.781 = 125.693 kN.m

Thickness of wall = 350mm

Effective depth = 350 – 40 – (8) = 302mm (assuming Y16mm bars will be employed for the construction)

k = M/(Fcubd2) = (125.693 × 106) / (30 × 1000 × 3022) = 0.0459
k < 0.156, no compression steel needed
la = 0.5 + (0.25 – k/0.9)0.5 = 0.5 + (0.25 – 0.0459/0.9)0.5 = 0.946
ASreq = M/(0.95Fy.la.d ) = (125.693 × 106) / (0.95 × 460 × 0.946 × 302) = 1006 mm2/m
ASmin = (0.13bh)/100 = (0.13 × 1000 × 350) / 100 = 455 mm2
Provide Y16 @ 150mm c/c (Asprov = 1340 mm2/m)

Check for shear
Design shear force on wall at ultimate limit state V = (1.4 × 66.064) = 92.4896 kN/m
Shear stress v = V/bd = (92.4896 × 1000) / (1000 × 302) = 0.3062 N/mm2

Vc = 0.632 (100As/bd)1/3 (400/d)1/4
Vc = 0.632 × [(100 × 1340)/(1000 × 302)]1/3 × (400/302)1/4
Vc = 0.632 × 0.7627 × 1.0727 = 0.517 N/mm2
For Fcu = 30N/mm2, Vc = 0.517 × (30/25)1/3 = 0.5494 N/mm2
Since v < Vc, no shear reinforcement required.

Design of the Base

The pressure distribution diagram on the base at serviceability limit state is as shown below;
qmax = P/B (1 + 6e/B) = 324.87/4 [1 + (6 × 0.0515)/(4)] = 87.491 kN/m2
qmin = P/B (1 – 6e/B) = 324.87/4 [1 – (6 × 0.0515)/(4)] = 74.927 kN/m2

Base%2BEarth%2BPressure

At ultimate limit state;
qmax = 1.4 × 87.491 = 122.487 KN/m2
qmin = 1.4 × 74.927 = 104.898 KN/m2

qC = 104.898 + [2.85 (122.487 – 104.898)]/4 = 117.430 kN/m2
qB = 104.898 + [3.2 (122.487 – 104.898)]/4 = 118.968 kN/m2

On investigating the maximum design moment about point C;

Back fill = 1.4 (18 × 5.1 × 2.85 × 2.85/2) = -521.952 kNm
Heel Slab = 1.4 (24 × 0.4 × 2.85 × 2.85/2) = -54.583 kNm
Earth Pressure = (104.898 × 2.85 × 2.85/2) + [(117.430 – 104.898) × 0.5 × 2.85 × 2.85/3] = 426.017 + 16.965 = 442.982 KNm
Net moment = -521.952 – 54.583 + 442.982 = -133.553 kNm

On investigating the maximum design moment about point B;

Back fill = (conservatively neglected)
Heel Slab = 1.4 (24 × 0.4 × 0.8 × 0.8/2) = – 4.3008 kNm
Earth Pressure = (118.968 × 0.8 × 0.8/2) + [(122.487 – 118.968) × 0.5 × 0.8 × (2 × 0.8/3)] = 37.9776 + 0.751 = 38.727 kNm
Net moment = -4.3008 + 38.727 = 34.426 kNm

Design of the toe
MB = 133.553 kN.m

Thickness of base = 400 mm

Effective depth = 400 – 50 – (8) = 342 mm (assuming Y16mm bars will be employed for the construction)

k = M/(Fcubd2) = (133.553 × 106) / (30 × 1000 × 3422) = 0.0385
k < 0.156, no compression steel needed
la = 0.5 + (0.25 – k/0.9)0.5 = 0.5 + (0.25 – 0.0385/0.9)0.5 = 0.95
ASreq = M/(0.95Fy.la.d ) = (133.553 × 106) / (0.95 × 460 × 0.95 × 342) = 941 mm2/m
ASmin = (0.13bh)/100 = (0.13 × 1000 × 400) / 100 = 520 mm2
Provide Y16 @ 175 mm c/c Top (Asprov = 1148  mm2/m)

Design of the heel
MC = 34.426 KNm

Thickness of base = 400 mm
Effective depth = 400 – 50 – (6) = 344 mm (assuming Y12mm bars will be employed for the construction)

k = M/(Fcubd2) = (34.426 × 106) / (30 × 1000 × 3442) = 0.00981
k < 0.156, no compression steel needed
la = 0.5 + (0.25 – k/0.9)0.5 = 0.5 + (0.25 – 0.00981/0.9)0.5 = 0.95
ASreq = M/(0.95Fy.la.d ) = (34.426 × 106) / (0.95 × 460 × 0.95 × 344) = 242 mm2/m
ASmin = (0.13bh)/100 = (0.13 × 1000 × 400) / 100 = 520 mm2
Provide Y12 @ 175mm c/c (Asprov = 646 mm2/m)

Check for shear at the base
The maximum shear force at ‘d’ from the face of the wall is investigated at the either side;

Maximum shear force at point B
Earth fill = 1.4 × 18 × 5.1 × 2.85 = -366.282 kN/m
Wall base = 1.4 × 24 × 0.4 × 2.85 = -38.304 kN/m
Base Earth Pressure = 0.5 (104.898 + 117.430) × 2.85 = 316.817 kN/m
Net shear force = -366.282 – 38.304 + 316.817 = -87.769 kN/m

A little investigation will show that this is the maximum shear force at any section on the base.

Taking the maximum shear stress at the base  v = (87.769 × 1000) / (1000 × 342) = 0.2566 N/mm2

Vc = 0.632 (100As/bd)1/3 (400/d)1/4
Vc = 0.632 × [(100 × 1148) / (1000 × 342)]1/3 × (400/342)1/4
Vc = 0.632 × 0.694 × 1.0399 = 0.456 N/mm2
For Fcu = 30N/mm2, Vc = 0.456 × (30/25)1/3 = 0.484 N/mm2
Since v < Vc, no shear reinforcement required.

DETAILING
I will need my readers to do the detailing sketches. I will accept both manual (hand) and CAD details. But your manual sketches must be very neat and well scaled. You should show the plans and at least one section. If your detailing is good enough, I will publish it on this post with your Facebook, LinkedIn, or G+ URL attached.

So, I will keep updating the post with as many good pictures as I receive. Good knowledge for all to flourish @ Structville

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Analysis of Arch-Frame Structure with Tie Element: A solved Example

An arch is supported on frame with different levels of supports as shown above. The frame is supported on a hinge at support A and a roller at support C. A tie beam is used to connect node B and support C. Plot the bending moment, shear force, and axial force diagram die to the externally applied load.

 
Solution

Support Reactions

∑MC = 0
30Ay – 10Ax  –  (10 × 302)/2 = 0
30Ay – 10Ax = 4500 ————- (1)

∑FX = 0
Ax + 25 = 0
Ax = -25 kN (pointing in the reverse of assumed direction)

Plugging the value of Ax into equation (1);
30Ay – 10(-25) = 4500
30Ay = 4250
Ay = 141.667 kN

∑MA = 0
30Cy  – (25 × 10) – (10 × 302)/2 = 0
30Cy = 4750
Cy = 158.333 kN

∑MDR = 0

15Cy –  (H × 5) – (10 × 152)/2 = 0
15(158.333) – 5H – (10 × 152)/2 = 0
– 5H + 1250 = 0
H = 250 kN

Arch Frame%2BSupport%2BReactions
Geometric Properties of the Arch Section

The ordinate of the arch at any given horizontal length section is given by;

y = [4yc (Lx – x2)] / L2

Where yc is the height of the crown of the arch
y = [(4 × 5) × (30x – x2)]/302 = (2/3)x – (x2/45)

dy/dx = y’ = 2/3 – 2x/45

At x = 0; y = 0
y’ = 2/3 – 0/8 = 0.667
sin⁡θ = y’/√(1 + y’2) = 1/√(1 + 0.6672) = 0.5546
cos⁡θ = 1/√(1 + y’2) = 1/√(1 + 0.6672) = 0.8319

At x = 7.5m;
y = (2/3)x – (x2/45) = (0.667 × 7.5) – (7.52/45) = 3.75m
y’ = 2/3 – 2(7.5)/45 = 0.333
sin⁡θ = y’/√(1 + y’2) = 0.333/√(1 + 0.3332) = 0.43159
cos⁡θ = 1/√(1 + y’2) = 1/√(1 + 0.3332) = 0.9487

At x = 15 m;
y = (2/3)x – (x2/45) = (0.667 × 15) – (152/45) = 5.00m
y’ = 2/3 – 2(15)/45 = 0
sin⁡θ = y’/√(1 + y’2) = 0/√(1 + 02) = 0
cos⁡θ = 1/√(1 + y’2) = 1/√(1 + 02) = 1.0

At x = 22.5m;
y = (2/3)x – (x2/45) = (0.667 × 22.5) – (22.52/45) = 3.75m
y’ = 2/3 – 2(22.5)/45 = -0.333
sin⁡θ = y’/√(1 + y’2) = -0.333/√(1 + 0.3332) = -0.43159
cos⁡θ = 1/√(1 + y’2) = 1/√(1 + 0.3332) = 0.9487

At x = 30m; y = 0
y’ = 2/3 – 2(30)/45 = -0.667
sin⁡θ = y’/√(1 + y’2) = -0.667/√(1 + 0.6672) = -0.5546
cos⁡θ = 1/√(1 + y’2) = 1/√(1 + 0.6672) = 0.8319


Internal Stresses in the Arch Structure
Bending Moment
MA = 0
MB= (25 × 10)  = 250 kN.m
MBUP = (25 × 10)  = 250 kN.m
M1 = (141.667 × 7.5) + (25 × 13.75) – (25 × 3.75) – (10 × 7.52)/2 – (250 × 3.75) = 93.7525 kN.m
MD = (141.667 × 15) + (25 × 15) – (25 × 5) – (10 × 152)/2 – (250 × 5) = 0

Coming from the right
M2 = (158.333 × 3.75) – (250 × 5) – (10 × 122)/2 = -31.252 kN.m
MC = 0



Shear force

Section A – B (Column)
Q– Ax = 0
Q–  25 = 0
Q– QBB  = 25  kN

Qi = ∑V cos⁡θ – ∑H sin⁡θ (for arch section)

Note that the horizontal forces of 25 kN will eliminate each other;

QBUP =  (141.667 × 0.8319) – (250 × 0.5546) = -20.797 kN
Q1R = Q1L = [141.667  – (10 × 7.5)] × 0.9487  – (250 × 0.43159) = -44.651 kN
QD =  [141.667 – (10 × 15)] × 1.0 – (250 × 0) = -8.333 kN
Q2R = Q2L =  [141.667 – (10 × 22.5)] × 0.9487 – (250 × –0.43159) = 28.839 kN
QC = [141.667 – (10 × 30)] × 0.8319 – (250 × -0.5546) = 6.932 kN

Axial force
Member AB = 141.667 kN (compression)
Member BC = 250 kN (Tension)

For the arch section;
Ni = -∑V sin⁡θ – ∑H cos⁡θ
NBUP = -(141.667 × 0.5546) – (250 × 0.8319) = -286.543 KN (Compression)
N1L = -[141.667 – (10 × 7.5)] × 0.43159 – (250 × 0.9487) = -265.848 KN
ND = -[141.667 – (10 × 15)] × 0 – (250 × 1) = -250 KN (Compression)
N2L = N3R = -[141.667 – (10 × 22.5)] × -0.43159 – (250 × 0.9487) = -273.141 KN
NC = -[141.667 – (10 × 30)] × -0.5546 – (250 × 0.8319) = -295.786 KN

Internal Stresses Diagram

Bending%2BMoment%2BDiagram
shear%2Bforce%2Bdiagram
Axial%2BForce%2BDiagram%2BArch Frame

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What is wrong with this section structural detailing?

A section of a beam profile is shown above. BASED ON THE GIVEN DATA ONLY AND WITHOUT MAKING ANY ASSUMPTIONS, identify the technical error(s) in the section detailing using BS 8110-1:1997 recommendations? Read the hints below carefully!

Data
Figured dimensions are in mm
Concrete cover at the sides and the soffit = 40 mm
Concrete cover at the top = 30 mm
Strength of reinforcement = 460 N/mm2
Strength of concrete = 35 N/mm2
Section is at mid-span (sagging moment)
Area of tension reinforcement required = 2960 mm2

Hints:
(1) This post is for educational purposes, hence, your reply is better dropped here on Structville as a comment so that every person accessing the post from different platforms can see the reply.

(2) Please, do not guess. If you identify the error(s), kindly drop your comment, otherwise, keep checking back for other people’s replies. Do not post your guesses.

(3) If you are not familiar with BS 8110-1:1997, but you identify any error based on the code that you are familiar with, kindly state the code, and the error you discovered. Try to be technical in your explanations, or quote the requirement as given in the code.

(4) The diagram is not to scale, so use the figured dimensions only. Also, do not call on any data or information that is not provided.

(5) Let your explanations be offered with love.

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Analysis and Design of Curved Circular Beams in a Reservoir

Beams that are curved in plan are often found in buildings, circular reservoirs, bridges, and other structures with curves. Curved beams always develop torsion (twisting) in addition to bending moment and shear forces because the center of gravity of loads acting normal to the plane of the structure lies outside the lines joining its supports. Therefore to maintain equilibrium in the structure, the supports of a curved beam must be fixed or continuous.

In this post, we are going to show in the most simplified manner, how to analyse continuous circular (ring) beams.

circular beam in a reservoir
Circular beam supporting an overhead water tank

For ring beams;
Maximum Negative Moment at any support = K1wr2
Maximum Positive Moment at any span = K2wr2
Maximum Torsional Moment = K3wr2
Total load on each column (support reaction) R = wr(2θ)

Shear force at any support = R/2 = wrθ

The coefficients are given in the table below;

Coefficients%2Bfor%2Bcurved%2Bbeams
Source: Table 21.1, Hassoun and Al-Manaseer (2008)

Solved Example
A cylindrical reservoir with a diameter of 6m is supported by a ring beam, which is supported on 8 equidistant columns. It is desired to analyse and design the ring beam to support the load from the superstructure.

The plan view of the structural disposition of the reservoir is shown below;

Curved%2BBeam%2Bplan%2Bview
reservoir%2Bsection

Load Analysis

(a) Geometry of sections
Dimension of beams = 450mm x 300mm
Dimension of column = ϕ300mm circular columns
Thickness of reservoir walls =  250mm
Thickness of reservoir slab = 250mm

(b) Density of materials
Density of stored material = 10 kN/m3
Density of concrete = 25 kN/m3

(c) Dead Loads
Weight of the walls = (25 kN/m3 × 0.25m × 4.75m × 18.849m) = 559.579 kN
Weight of bottom slab = (25 kN/m3 × 0.25m × 28.274m2) = 176.7125 kN
Weight of water stored = (10 kN/m3 × 4.5m × 23.758m2) = 1069.11 KN
Total = 1805.4015 kN

Let us transfer this load to the the ring beam based on the perimeter.

Perimeter of ring beam = πd = π × 6 = 18.849m

w = 1805.4015 kN / Perimeter of ring beam = 1805.4015 kN / 18.849m = 95.782 kN/m

Self weight of the beam = 25 kN/m3 × 0.3m × 0.45m = 3.375 kN/m

Total dead load on beam = 95.782 kN/m + 3.375 kN/m = 99.157 kN/m

Factoring the load on the beams at ultimate limit state = 1.35 × 99.157 kN/m = 133.862 kN/m

Circular%2Bbeam%2Bcarring%2BUDL

From the table above;
Number of supports (n) = 8
θ = π/n = 45°
K1 = 0.052
K2 = 0.026
K3 = 0.0040
Radius (r) = 3m

Maximum Negative Moment at the supports = K1wr= -0.052 × 133.862 × 32 = -62.647 KN.m

Maximum Positive Moment at the spans = K2wr= 0.026 × 133.862 × 32 = 31.323 KN.m

Maximum Torsional Moment = K3wr= 0.0040 × 133.862 × 32 = 4.819 KN.m

Shear force at the supports = R/2 = wrθ = 133.862 × 3 × (π/8) = 157.7 KN


Structural Design
Design strength of concrete fck = 35 N/mm2
Yield strength of reinforcement fyk = 500 N/mm2
Nominal cover to reinforcement = 30 mm

Span
MEd = 31.323 kN.m

Effective depth (d) = h – Cnom – ϕ/2 – ϕlinks
Assuming ϕ12 mm bars will be employed for the main bars, and ϕ8mm bars for the stirrups (links)
d = 450 – 30 – 6 – 8 = 406 mm

k = MEd/(fckbd2) = (31.323 × 106)/(35 × 300 × 4062) = 0.0181
Since k < 0.167, no compression reinforcement required
z = d[0.5+ √(0.25 – 0.882K) ] = z = d[0.5+ √(0.25 – 0.882(0.0181))] = 0.95d

As1 = MEd/(0.87yk z) = (31.323 × 106)/(0.87 × 500 × 0.95 × 406) = 186.69 mm2
Provide 3H12 mm BOT (ASprov = 339 mm2)

Supports
MEd = 62.647 KN.m

Effective depth (d) = h – Cnom – ϕ/2 – ϕlinks
Assuming ϕ16 mm bars will be employed for the main bars, and ϕ8mm bars for the stirrups (links)
d = 450 – 30 – 8 – 8 = 404 mm

k = MEd/(fckbd2) = (62.647 × 106)/(35 × 300 × 4042) = 0.0365
Since k < 0.167, no compression reinforcement required
z = d[0.5+ √(0.25 – 0.882K) ] = z = d[0.5+ √(0.25 – 0.882(0.0365))] = 0.95d

As1 = MEd/(0.87fyk z) = (62.647 × 106)/(0.87 × 500 × 0.95 × 404) = 375.23 mm2
Provide 2H16 mm TOP (ASprov = 402 mm2)

Interaction of shear and torsion
According to clause 6.3.2(2) of Eurocode 2, the effects of torsion and shear for both hollow and solid members may be superimposed, assuming the same value for the strut inclination θ. The limits for θ given in 6.2.3 (2) of EC2 are also fully applicable for the case of combined shear and torsion.

According to clause 6.3.2(4) of EC2, the maximum resistance of a member subjected to torsion and shear is limited by the capacity of the concrete struts. In order not to exceed this resistance the following condition should be satisfied:

TEd /TRd,max + VEd /VRd,max ≤ 1 ———- Equation (6.29 of EC2)

VEd = 157.7 KN
TEd = 4.819 kN.m
TRd,max = design torsional resistance moment
VRd,max = maximum shear resistance of the cross-section

Geometrical Properties for analysis of torsion
Area (A) = 300mm × 450mm = 135000 mm2
Perimeter (U) = 2(300) + 2(450) = 1500mm
Equivalent thickness = tef,i = A/U = 135000/1500 = 90mm

The equivalent thin wall section for the rectangular section is given below;

Equivalent%2Bthin%2Bwall%2Bsection

A= the area enclosed by the centre-lines of the connecting walls, including inner hollow areas = (450 – 90) × (300 – 90) = 75600 mm2
U= is the perimeter of the area Ak = 2(450 – 90) + 2(300 – 90) = 1140 mm

TRd,max = 2 v αcwfcdAktef,i sinθ cosθ

Assuming θ = 21.8° (cot θ = 2.5)
v = 0.6(1 – fck/250) = 0.6(1 – 35/250) = 0.516
fcd = (αcc × fck)/γc = (1 × 35)/1.5 = 23.33 N/mm2

TRd,max = 2 × 0.516 × 1.0 × 23.33 × 75600 × 90 × cos 21.8° × sin 21.8° × 10-6 = 56.485 KNm

VRd,c = [CRd,c.k.(100ρ1 fck)(1/3) + k1cp]bw.d

Where;
CRd,c = 0.18/γc = 0.18/1.5 = 0.12
k = 1 + √(200/d) = 1 + √(200/404) = 1.704 > 2.0, therefore, k = 1.702
ρ1 = As/bd = 402/(300 × 404) = 0.003317 < 0.02; K1 = 0.15

VRd,c = [0.12 × 1.704(100 × 0.003317 × 35 )(1/3)] 300 × 404 = 65469.358 N = 65.469 KN

Since VRd,c (65.469 KN) < VEd (157.7 KN), shear reinforcement is required.

The compression capacity of the compression strut (VRd,max) assuming θ = 21.8° (cot θ = 2.5)

VRd,max = (bw.z.v1.fcd)/(cot⁡θ + tanθ)
V1 = 0.6(1 – fck/250) = 0.6(1 – 35/250) = 0.516
fcd = (αcc ) fck)/γc = (1 × 35)/1.5 = 23.33 N/mm2
Let z = 0.9d

VRd,max = [(300 × 0.9 × 404 × 0.516 × 23.333)/(2.5 + 0.4)] × 10-3 = 452.863 KN

Since VRd,c < VEd < VRd,max
Hence, Asw/S = VEd/(0.87Fykzcot θ) = 157700/(0.87 × 500 × 0.9 × 404 × 2.5 ) = 0.3988

Minimum shear reinforcement;
Asw/S = ρw,min × bw × sinα (α = 90° for vertical links)
ρw,min = (0.08 × √(fck))/fyk = (0.08 × √35)/500 = 0.0009465
Asw/S (min) = 0.0009465 × 300 × 1 = 0.2839
Since 0.2839 < 0.3988, adopt 0.3988

Maximum spacing of shear links = 0.75d = 0.75 × 404 = 303mm
Provide H8mm @ 250mm c/c (Asw/S = 0.402) Ok

Note that this link must be properly closed with adequate anchorage length, because it will assist in resisting torsion.

Design Considerations for Torsion
TEd /TRd,max + VEd /VRd,max ≤ 1

(4.891/56.485) + (157.7/453.863) = 0.434 < 1.0 Hence it is ok

However, note that the actual shear force at the point where torsion is maximum is actually less than the shear force at the support. The relationship above is an error but on the safe side.

The maximum torsion occurs at an angle of 9.5° from the support (see Table above). Therefore, the actual shear force at that section ( VEd) = Shear force at support – wrα

VEd = 157.7 – (133.862 × 3 × (9.5/180)  × π) = 91.114 KN

Therefore for educational purposes, this is the shear force that should be used to check the shear-torsion interaction. A little consideration will show that  VRd,max  is constant all through the section, but VRd,c  might vary depending on the longitudinal reinforcement provided at the section.

Rechecking the interaction above;

(4.891/56.485) + (91.114/453.863) = 0.287< 1.0 Hence it is ok

Area of transverse reinforcement to resist torsion
Asw/s = TEd/2Ak fyw,d cotθ
Asw/s = (4.819 × 106) / (2 × 135000 × 0.87 × 500 × 2.5) = 0.0164 < Asw/S (min)
Therefore, links provided for shear will be adequate for resisting torsion.

Area of longitudinal reinforcement to resist torsion
As1 = TEdUk cot θ / 2Ak fyd
As1 = (4.819 × 106 × 1140 × 2.5) / (2 × 75600 × 0.87 × 500) = 208 mm2

According to clause 6.3.2(4), in compressive chords, the longitudinal reinforcement may be reduced in proportion to the available compressive force. In tensile chords the longitudinal reinforcement for torsion should be added to the other reinforcement. The longitudinal reinforcement should generally be distributed over the length of side, but for smaller sections it may be concentrated at the ends of this length.

However, for the avoidance of doubt since no definition was given for what could be regarded as a ‘smaller section’, Provide 1H12mm bar at the middle of the section at both faces. The tensile and longitudinal reinforcement provided at the top and bottom of the section should be able to take care of the rest.

SECTION%2BAT%2BSUPPORT
SECTION%2BAT%2BSPAN

Further information
Nominal shear reinforcement is required in rectangular sections when;

TEd /TRd,c + VEd /VRd,c ≤ 1 ————– Equation (6.31 of EC2)

Where;
TRd,c is the value of the torsion cracking moment:
VRd,c is as defined above.

TRd,c = fctd⋅t⋅2Ak
τ = fctd = fctk /γc = 2.2/1.5 = 1.466 MPa (fctk deducted from Table [3.1 – EC2]).

It results therefore:
TRd,c = fctd⋅t⋅2Ak = 1.466 × 90 × 2 × 75600 × 10-6 = 19.949 kNm

From above calculations;
VRd,c = [0.12 × 1.704(100 × 0.003317 × 35 )(1/3)] 300 × 404 = 65469.358 N = 65.469 KN

(4.819/19.949) + 91.114/65.469) = 1.633 > 1.0 (Shear force at point of maximum torsion was used)

Therefore obviously this showed that shear reinforcement calculations were required.

References
Hassoun M.N., Al-Manaseer A. (2008): Structural Concrete Theory and Design (4th Edition). John Wile and Son Inc., New Jersey

Preparation of Bar Bending Schedule For Floor Slabs

Bar bending schedule is an important structural working document that shows the disposition, bending shape, total length, and quantity of all the reinforcements that have been provided in a structural drawing. It is often provided in a separate sheet (usually A4 paper) from the structural drawing. The bar marks from structural detailing drawing are directly transferred to the bar bending schedule. We normally quantify reinforcements based on their total mass in tonnes or kilograms. For smaller projects, you can quantify based on the number of lengths needed.

Bar bending schedule is prepared for floor slabs to show the quantity, size, and shape of rebars needed during the construction. This document is very important for pre-contract and post-contract operations. The information needed for the preparation of bar bending schedule for floor slab is picked from the reinforcement detailing drawings. One important parameter in the preparation of bar bending schedule is the quantity of steel required (in kilograms or tonnes). This is based on the unit mass and size of the rebars.

Unit mass of rebars

The unit mass of the reinforcements are derived from the density of steel. The density of steel normally used for this purpose is 7850 kg/m3.

For example, let us consider 12mm bar;
The area is given by (πd2)/4 = (π × 122)/4 = 113.097mm2 = 0.0001131m2
Considering a unit length of the bar, we can verify that the volume of a metre length of the bar is 0.0001131m3;

Density = Mass/Volume = 7850 kg/m3 = Mass/0.0001131
Therefore, the unit mass of 12mm bar = 7850 × 0.0001131 = 0.888 kg/m

Therefore for any diameter of bar;
Basic weight = 0.00785 kg/mm2 per metre
Weight per metre = 0.006165 ϕ2 kg
Weight per mm2 at spacing s(mm) = 6.165ϕ2/s kg

Where;
ϕ = diameter of bar in millimetres

The unit weight of different types of reinforcement sizes is given in the Table below;

Diameter of bar (mm)Weight per metre (kg)Length per tonne (m)
60.2224505
80.3952532
100.6161623
120.8881126
161.579633
202.466406
253.854259
326.313158
409.864101


Basic Shapes
for Bar Bending Schedule

There are some basic shape codes in the code of practice (BS 8666:2005). But these days, it is common to sketch the bending shape on the BBS document to avoid the confusion and extra effort that comes with extracting the shape from a standard document.

To obtain the length of reinforcement bars in a structural drawing, use the following relation;

Length of bar = Effective Length + Width of Support – Concrete cover (s) – Tolerances

The typical values of tolerances (deductions) are given in the table below;

Deductions%2Bfor%2Bbending%2Bschedule

Example on the Preparation of the Bar Bending Schedule of a Slab


To illustrate how this is done, consider the general arrangement of the first floor of a building as shown below;

floor%2Bplan%2Bbending
SLAB%2BDET%2B2
SECTION

Bar Bending Schedule Calculations

SHAPE%2BCODE%2B38

Cutting Length of reinforcement = A + B + C – r – 2d (Table 2.19, Reynolds, Steedman, and Threlfall, 2008)

Where;
r = radius of bend (r = 24 mm for high yield 12 mm bars; and 20 mm for Y10mm bars)
d = diameter of bar

Bar Mark 01:
A  = 4000 + 230 – 35 = 4195 mm
B = 150 – 2(25) – 10 = 90 mm (including 10 mm tolerance)
C = 230 + 800 – 35  = 995 mm (from detailing considerations 0.2L)
r = 24 (for 12 mm bars)

L = A + B + C – r – 2d = 4195 + 90 + 995 – 24 – 2(12) = 5235 mm

 
 
01

Bar Mark 02:
L = 2230 mm

02



Bar Mark 03:
A  = 3600 + 230 – 35 = 3795 mm
B = 150 – 2(25) – 12 – 10 = 78 mm (including 10 mm tolerance)
C = 230 + 720 – 35  = 915 mm (from detailing considerations 0.2L)
r = 24 (for 12 mm bars)

L = A + B + C – r – 2d = 3795 + 78 + 915 – 24 – 2(12) = 4740 mm

03

Bar Mark 04:
A  = 1080 1200 + 230 – 25 = 2485 mm
B = 150 – 2(25) – 10 = 90 mm (including 10 mm tolerance)
C = 1200 + 230 – 25 = 1405 mm (from detailing considerations 0.2L)
r = 24 (for 12 mm bars)

L = A + B + C – r – 2d = 2485 + 1405 + 90 – 24 – 2(12) = 3932 mm

04

Bar Mark 05:
A  = 6000 + 230 – 35 = 6195 mm
B = 150 – 2(25) – 12 – 10 = 78 mm (including 10 mm tolerance)
C = 1200 + 230 – 35 = 1395 mm (from detailing considerations 0.2L)
r = 20 (for 10 mm bars)

L = A + B + C – r – 2d = 6195 + 1395 + 78 – 20 – 2(10) = 7628 mm

05

Bar Mark 06:
L = 4630 mm

06



Bar Mark 07:

L = 3830 mm

07


Bar Mark 08:
A  = 1200 + 230 – 35 – 25 – (15) = 1355 mm (including 15 mm tolerance)
B = 150 – 2(25) – 10 = 90 mm (including 10 mm tolerance)
r = 24 (for 12 mm bars)

L = 2(A) + 2(B) + C + D – 3r – 6d = 2(1355) + 2(90) + 2(125) – 3(24)  – 6(12) = 2996 mm

FINAL



Bar Mark 09:
L = 2030 mm

09

Bar Mark 10:
L = 1830 mm

10

The final table for the bar bending schedule can be prepared as shown below. However, it is important to include all details in the schedule to avoid confusion.

Bar%2BBending%2BSchedule%2BTable

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How to Carry Out Concrete Mix Design

Concrete mix design is the process of specifying and proportioning the quantity of concrete ingredients (cement, sand, gravel, and water) required to produce concrete with a specified fresh and hardened properties. Nowadays, engineers should have a deeper understanding of concrete mixes, than just specifying say 1:2:4 concrete mix ratio for their construction works.

Under normal and well-controlled conditions, 1:2:4 mix ratio should yield concrete with 28 days compressive strength greater than 20 N/mm2. However, there are variations in results when batching by weight and when batching by volume. This situation demands that to produce concrete of a specified compressive strength, you have to accurately carry out concrete mix design, which incorporates the tendency of failure during tests.

A little consideration from concrete mix design results will show that the mix ratio for batching by weight, and for batching by volume are not basically the same for obtaining a specified grade of concrete.

Ingredients for concrete mix design
Figure 1: Basic ingredients for concrete production.

The compressive strength of concrete is a very variable quantity. Therefore, when carrying out a concrete mix design, it is important to target a higher average strength so that every part of the structure will meet the specified strength. Statistical standard deviation which is a measure of scatter or dispersion of strength about the mean is normally used to take care of this.

The target strength of concrete (fm) during mix design is given by;

fm = fmin + KSD ————– (1)

Where;

  • fm is the mean compressive strength
  • fmin is the minimum compressive strength of the concrete. In the Eurocodes, this is called the characteristic strength of the concrete (fck), while in the US, it is called the design strength (fc‘).
  • K is the probability factor which is usually taken as 1.64 or 2.33 to express the probability of 1 in 20 and 1 in 100 respectively, for the strength to fall below the minimum strength.
  • SD is the standard deviation which is best obtained by considering the previous test results obtained using the same materials, the same procedure, and under the same supervision.

The term KSD is normally referred to as the margin.

The probability of strength values in the range fck ± KSD and below fck – KSD (risk) for normal distribution is shown in Table 1.0 below;

Table 1: The probability of strength values in the range fck ± KSD and below fck – KSD (risk) for normal distribution (Neville and Brooks, 2010)

Probability factor (k)Probability of strength values in the range fck ± KSD (%)Probability of strength values below fck – KSD (%)
1.0068.215.9 (1 in 6)
1.6490.05.0 (1 in 20)
1.9695.02.5 (1 in 40)
2.3398.01.0 (1 in 100)
3.0099.70.15 (1 in 700)

In the Eurocodes and in many other codes, the range of the risk of 1 in 20 is recommended for concrete tests. This means that in 20 concrete cubes, there is a probability of only one cube not meeting the required strength. When statistical data is not available for obtaining the standard deviation, the values in table 2 according to ACI code could be used.

Table 2: Required average compressive strength when data is not available to establish a standard deviation

Specified Compressive strength f’c (MPa)Required Average Compressive Strength f’cr (MPa)
Less than 21f’c + 7.0
21 to 35f’c + 8.5
Over 351.10f’c + 5

The process of carrying out concrete mix design are as follows;

  1. Test the materials to be used for the concrete mix design. For the aggregates, it is important to obtain the oven-dry relative density, fineness modulus, absorption, and bulk density.
  2. Establish the target strength of the concrete at 28 days by considering the characteristic strength and the margin which is based on the standard deviation.
  3. Establish the required water-cement cement ratio for the target strength using relevant tables
  4. Calculate the water requirement for the desired slump using relevant tables
  5. Use the calculated water content to calculate the cement content using the water-cement ratio relationship
  6. Calculate the mass of coarse aggregates using the bulk volume of coarse aggregate per unit volume of concrete
  7. Calculate the mass of fine aggregates
  8. Summarise your results

Worked Example

Let us consider the trial mix design for a concrete of minimum specified strength of 25 N/mm2, to be employed in the construction of the floor beams and slab of a building.

Materials Analysis
Coarse aggregate: Crushed granite of nominal maximum size of 20mm
Oven dry relative density = 2.68
Fineness modulus = 2.60
Absorption = 0.4% (saturated surface dry)
Bulk density = 1650 kg/m3

Specific gravity of cement = 3.15

Fine aggregate: Sharp sand from river
Relative density = 2.64
Absorption = 0.60 %
Bulk density = 1600 kg/m3

The target strength can be obtained from the relation below;
fm = fck + KSD
fm = 25 + 8.5 = 33.5 N/mm2

Water-Cement Ratio

The relationship between the water to cement ratio for non-air-entrained concrete (normal concrete) and the 28 days compressive strength is given in Table 3.

Table 3: Relationship between compressive strength and water to cement ratio

Compressive strength at 28 days (MPa)Water to cement ratio by mass
450.38
400.42
350.47
300.54
250.61
200.69
150.79



Therefore, Water – Cement ratio for non-air entrained 33.4 N/mm2 concrete = 0.491 (interpolating from Table 3)

Cement and Water Content
Water content is normally estimated from workability requirements, which is guided by the slump. The range of slump required for different types of construction is given in Table 4;

Table 4: Different slumps for different types of construction works

Concrete ConstructionMaximum slump (mm)Minimum slump (mm)
Reinforced foundation walls and footings7525
Plain footings, caissons, and substructure walls7525
Beams and reinforced walls10025
Columns in buildings10025
Pavements and slabs7525
Mass cocrete7525

For maximum size of aggregate of 19mm, and a slump of 75mm, the Table 5 gives a water demand of 205 kg/m3



Table 5: Approximate mixing water and target air content requirements for different slumps and nominal maximum sizes of aggregate

SlumpWater content (kg/m3) for 9.5 mm aggregate sizeWater content (kg/m3) for 12.5 mm aggregate sizeWater content (kg/m3) for 19 mm aggregate sizeWater content (kg/m3) for 25 mm aggregate sizeWater content (kg/m3) for 37.5 mm aggregate sizeWater content (kg/m3) for 50 mm aggregate sizeWater content (kg/m3) for 75 mm aggregate sizeWater content (kg/m3) for 150 mm aggregate size
25 – 50207199190179166154130113
75 – 100228216205193181169145124
150 -175243228216202190178160
Approximate amount of entrapped air (%)32.521.510.50.30.2

Therefore cement content;
205/C= 0.491; Therefore the cement content (C) = 205 / 0.491 = 417.515 kg/m3

Mass of Coarse Aggregates


For 19mm aggregate with a fineness modulus of 2.60, the bulk volume of dry rodded coarse aggregate per m3 of concrete is 0.64 (see Table 6).

Table 6: Bulk volume of coarse aggregate per unit volume of concrete

Nominal maximum size of aggregate (mm)Bulk volume
(2.40 fineness modulus)
Bulk volume
(2.60 fineness modulus)
Bulk volume
(2.80 fineness modulus)
Bulk volume
(3.0 fineness modulus)
9.50.500.480.460.44
12.50.590.570.550.53
190.660.640.620.60
250.710.690.670.65
37.50.750.730.710.69
500.780.760.740.72
750.820.800.780.76
1500.870.850.830.81

Therefore, mass of coarse aggregate (Mc) per m3 of concrete = 0.64 × 1650 = 1056 kg/m3

Approximate air content = 2%

Mass of fine aggregates

The mass of coarse aggregate can be estimated using the relationship below;

Mass of fine aggregate Mf = γf [1000 – (W – C/γ + Mc/γc + 10A)] ————- (2)

Where;
γf = Specific gravity of fine aggregate (saturated surface dry)
W = Mixing water requirement
C = Cement Content
γ = Specific gravity of cement (take value as 3.15 unless otherwise specified)
Mc = Coarse Aggregate content
γc = Specific gravity of coarse aggregate (saturated surface dry)
A = Air content (%)

Therefore:
Mf = 2.64 [1000 – (205 + (417.515/3.15) + (1056/2.68) + (10 × 2))] = 655.843 kg/m3

Final Volume computations
Water = 205 / (1 × 1000) = 0.205 m3
Cement = 417.515 / (3.15 × 1000) = 0.1325 m3
Air = 2/100 = 0.02
Coarse aggregate = 1056 / (2.68 × 1000) = 0.394 m3
Fine aggregate = 655.843 / (2.64 × 1000) = 0.248 m3

SUMMARY OF TRIAL MIX DESIGN
By weight
Water = 205 kg/m3
Cement = 417.515 kg/m3
Coarse Aggregate = 1056 kg/m3
Fine Aggregate = 655.843 kg/m3

Yield of concrete = 2334.36 kg/m3

Mix ratio by weight (Cement : Fine Aggregate : Coarse Aggregate) = (1:1.57:2.53)

By volume
Water = 0.205 m3
Cement = 0.1325 m3
Coarse Aggregate = 0.394 m3
Fine Aggregate = 0.248 m3

Mix ratio by volume (Cement : Fine Aggregate : Coarse Aggregate) = (1:1.87:2.97)

MIX DESIGN WITHOUT CONSIDERING TEST MARGIN
However, carrying out mix design for 25 N/mm2 grade of concrete without considering the margin, we can obtain the following result using the steps described above;

Water-cement ratio
Water – Cement ratio for non-air entrained 25 N/mm2 concrete = 0.61 (see Table 3 above)

Water and Cement Demand
For maximum size of aggregate of 19mm, and a slump of 75mm, gives a water demand of 205 kg/m3.
Therefore the cement content C = 205/0.61= 336.06 kg/m3

Mass of Coarse Aggregate
For 19mm aggregate with fineness modulus of 2.60, the bulk volume of dry rodded coarse aggregate per m3 of concrete is 0.64. Therefore;
Weight per m3 = 0.64 × 1650 = 1056 kg/m3

Approximate air content = 2%

Mass of Fine Aggregate
Mass of fine aggregate Mf = γf [1000 – (W – C/γ + Mc/γc + 10A)]
Mf = 2.64 [1000- (205 + (336.06/3.15) + (1056/2.68) + 10(2))] = 724.11 kg/m3

Volume computations
Water = 205 / (1 × 1000) = 0.205 m3
Cement = 336.06 / (3.15 × 1000) = 0.1066 m3
Air = 2/100 = 0.02%
Coarse aggregate = 1056 / (2.68 × 1000) = 0.394 m3
Fine aggregate = 724.11 / (2.64 × 1000) = 0.274 m3

Summary of trial mix design without considering the margin
By weight
Water = 205 kg/m3
Cement = 336.06 kg/m3
Coarse Aggregate = 1056 kg/m3
Fine Aggregate = 724.11 kg/m3
Yield of concrete = 2321.17 kg/m3
Mix ratio by weight (Cement:Fine Aggregate:Coarse Aggregate) = (1: 2.15: 3.142)

By volume
Water = 0.205 m3
Cement = 0.1066 m3
Coarse Aggregate = 0.394 m3
Fine Aggregate = 0.274 m3
Mix ratio by volume (Cement:Fine Aggregate:Coarse Aggregate) = (1:2.57:3.696)

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Design of Biaxial Reinforced Concrete Columns

A biaxial column is a column that is subjected to compressive axial force and bending moment in the two planes. They are usually found at the corners of a building or at locations where the beam spans and/or loading are not equal. In the design of biaxial reinforced concrete columns, a non-linear analysis method is required, which should take into account second-order, imperfection, and biaxial bending effects.

Biaxial Reinforced Concrete Columns
The columns circled in red are biaxially loaded

EN 1992-1-:2004 (Eurocode 2) did not give an express method of designing biaxial columns other than working from the first principles. This may not be very easy to achieve without the use of charts or computer programs. To develop such a program, one can divide the compression zone into strips that are parallel with the neutral axis of the section, and calculate the stress in each strip using the parabolic-rectangular diagram. The force and moment at each strip in the x and y-axis can be summed up in the ultimate limit state to find the moment and axial force developed by the concrete in compression.

There are however simplified methods of dealing with biaxial bending in reinforced concrete structures. An example is the approach given in clause 5.8.9(4) of EN 1992-1-1 for the design of biaxially bent sections in slender columns. This is based on the observation that the form of the Mx – My interaction diagram can conveniently be represented by a super-ellipse. A super-ellipse has an equation of the form;

xa + ya = k —— (1)

If a = 2, this equation becomes a circle, while if a = 1 it describes a straight line. At loads approaching the squash load, the Mx – My interaction diagram approaches a circle, while in the region of the balance point it is close to a straight line. Clause 5.8.9(4) adopts the equation below as a means of describing the complete interaction surface;

(ME,dz/MR,dz )a + (MEd,y/MRd,y )a ≤ 1.0 —— (2)

The proximity to the squash load can be defined using the N/Nuz ratio parameter, and EN 1992-1-1 assumes the relationship between this parameter and the exponent ‘a‘ given in the Table below. Intermediate values may be interpolated.

NEd/NRd0.10.71.0
a1.01.52.0

In the Table above, NRd is the squash load of the column, and may be calculated from

NRd = Acfcd + Asfyd —— (3)

The difficulty with the approach from the practical point of view is that it cannot be used as a direct design method since NRd can only be established once the reinforcement area has been found. It, therefore, has to be used iteratively. An initial estimate is made of N/Nuz, the section is designed, a corrected value of N/Nuz can then be estimated, and the process repeated until a correct solution is obtained.

A much simpler, but considerably more approximate method to the design of biaxial columns has been adopted in BS 8110. The design is carried out for an increased uniaxial moment, which takes account of the biaxial effects. The required uniaxial moment is obtained from whichever is appropriate of the two relationships set out below:

if Mx/h’ > My/b’ then M’x = Mx + βh’My/b’ —— (4)
if Mx/h’ < My/b’ then M’y = My + βb’Mx /h’ —— (5)

In the above relationships, Mx and My are the design moments about the x and y axes, respectively, while M’x and M’y are the effective uniaxial moments for which the section is actually designed. b’ and h’ are the effective depths of the column section (see image below). The factor β is defined in BS 8110 as a function of N/bhfcu. In terms of fck, it can be obtained from the relationship;

β = 1 – N/bhfck (0.3 < β < 1.0) —— (6)

BIAXIALLY%2BBENT%2BCOLUMN%2B%2528BS%2B8110%2529

This approach has the great advantage of being very simple. It is, however, an approximate approach.

Example on the Design of Biaxial Reinforced Concrete Columns to BS 8110 and Eurocode 2

A reinforced concrete column fixed at both ends is subjected to the loading condition shown below. We are required to obtain the appropriate longitudinal reinforcement for the column using BS 8110-1:1997 and Eurocode 2.

The column is carrying longitudinal and transverse beams of depth 600mm and width 300mm. It is also supported by beams of the same dimension. The centre to centre height of the column is 3500mm. The plan view of the arrangement of the beams and column is as shown below.

BIAXIAL%2BCOLUMN

DESIGN ACCORDING TO BS 8110-1:1997
N = 716.88 kN;
TOP: Mx-x = 175.87 kNm; My-y = 35.52 kNm
BOTTOM: Mx-x = -85.832 kNm; My-y = -25.269 kNm

Concrete grade fcu = 30 N/mm2
Yield Strength of reinforcement fy = 460 N/mm2
Concrete cover = 40mm
Lo = 3.5m, Effective length Le = 0.75 × (3500 – 600) = 2175 mm;
Size of column = 400 x 300mm;
Slenderness = 2175/300 = 7.25 < 15. Thus column is short.

Effective depth about x-x axis
h’ = (400 – 40 – 12.5 – 10) = 337.5 mm

Effective depth about y-y axis
b’ = (300 – 40 – 12.5 – 10) = 237.5 mm

Mx/h’ = 521.109 kN; My/ b’ = 149.558  kN

Axial-load ratio

Nratio = (N × 1000) / (Fcu × b × h) = (716.88 × 1000) / (30 × 400 × 300) = 0.1991

From Table 3.22 of BS 8110-1:1997, for Nratio = 0.1991
Therefore, β = 1 – 1.1644(0.1991) = 0.7681

As Mx/h’ exceeds My/b’
Mx‘ = Mx + βh’/b’My
Mx‘ = 175.87 + [0.7681 × (0.3375)/(0.2375 ) × 35.52] = 214.64 kNm

Minimum Eccentricity in Columns
According to clause 3.8.2.4 of BS 8110-1:1997, at no section in a column should the design moment be taken as less than that produced by considering the design ultimate axial load as acting at a minimum eccentricity, emin equal to 0.05 times the overall dimension of the column in the plane of bending considered but not more than 20 mm.

Where biaxial bending is considered, it is only necessary to ensure that the eccentricity exceeds the minimum about one axis at a time.

In the x-x direction = emin = 0.05 × 400 = 20mm, therefore adopt 20mm, Mx = 716.88 × 0.02 = 14.3376 kNm < 214.64 kNm

In the y-y direction = emin = 0.05 × 300 = 15mm, therefore adopt 15mm, My = 716.88 × 0.015 = 10.7532 kNm < 214.64 kNm

Section design ratios for chart entry

Axial load ratio Nratio = (N × 1000)/(Fcu × b × h) = (716.88 × 1000)/(30 × 400 × 300) = 0.1991

Mratio = M/(Fcu × b × h2) = (214.64 × 106) / (30 × 300 × 4002) = 0.149

With d’/h = 337.5/400 = 0.84375

column%2Bdesign%2Bchart%2Bbs%2B8110

From chart, (ρ × Fy)/(Fcu) = 0.286 Therefore, ρ = (0.286 × 30) / 460 = 0.01865
ASCreq = 0.01865 × 400 × 300 = 2238.26 mm2

Provide 6Y25mm (Asprov = 2946 mm2)
Maximum area of reinforcement = 0.06bh = 0.06 × 400 × 300 = 7200 mm2

DESIGN ACCORDING TO EUROCODE 2
Clause 5.8.9(2) of EN 1992-1-1:2004 permits us to perform separate designs in each principal direction, disregarding biaxial bending as a first step. Imperfections need to be taken into account only in the direction where they will have the most unfavourable effect. However, in this example, we have carried out imperfection analysis in both directions.

NEd = 716.88 KN

Elastic Moments
Y – direction: M01 = 175.87 kNm; M02 = -85.832 kNm
Z – direction: M01 = 35.52 kNm; M02 = -25.269 kNm

Clear column height (L) = 3500 – 600 = 2900 mm

Calculation of the effective height of the column (Lo)
Let us first of all calculate the relative stiffnesses of the members in the planes of bending.

In the y-direction;
Second moment of area of beam 1 (I1) = bh3/12 = 0.3 × 0.63/12 = 0.0054 m4
Stiffness of beam 1 (since E is constant) = 4I1/L = (4 × 0.0054) / 6 = 0.0036

Second moment of area of beam (I2) = bh3/12 = 0.3 × 0.63/12 = 0.0054 m4
Stiffness of beam 2 (since E is constant) = 4I2/L = (4 × 0.0054) / 3.5 = 0.00617

Second moment of area of column (Ic) = bh3/12 = 0.0016 m4
Stiffness of column = 4Ic/L = (4 × 0.0016) / 3.5 = 0.001828

For compression members in regular braced frames, the slenderness criterion should be checked with an effective length l0 determined in the following way:

Lo = 0.5L √[(1 + k1)/(0.45 + k1)) × (1 + k2)/(0.45 + k2))]

Where;
k1, k2 are the relative flexibilities of rotational restraints at ends 1 and 2 respectively
L is the clear height of the column between the end restraints

k = 0 is the theoretical limit for rigid rotational restraint, and k = ∞ represents the limit for no restraint at all. Since fully rigid restraint is rare in practise, a minimum value of 0.1 is recommended for k1 and k2.

In the above equations, k1 and k2 are the relative flexibilities of rotational restraint at nodes 1 and 2 respectively. If the stiffness of adjacent columns does not vary significantly (say, the difference not exceeding 15% of the higher value), the relative flexibility may be taken as the stiffness of the column under consideration divided by the sum of the stiffness of the beams (or, for an end column, the stiffness of the beam) attached to the column in the appropriate plane of bending.

Remember that we will have to reduce the stiffness of the beams by half to account for cracking;

k1 = k2 = 0.001828 / (0.0018 + 0.003085) = 0.3743

Lo = 0.5 × 2900√[((1 + 0.3743)/(0.45 + 0.3743)) × (1 + 0.3743)/(0.45 + 0.3743)] = 2647.77 mm

Compare with BS 8110’s 0.75L = 0.75 × 2900 = 2175 mm

In the z-direction
;
Second moment of area of beam 3 (I3) = bh3/12 = 0.3 × 0.63/12 = 0.0054 m4
Stiffness of beam 3 (since E is constant) = 4I1/L = (4 × 0.0054) / 3.5 = 0.00617

Second moment of area of column (Ic) = bh3/12 = 0.0009 m4
Stiffness of column = 4Ic/L = (4 × 0.0009) / 3.5 = 0.00102857

k1 = k2 = 0.00102857/(0.003085) = 0.3334

lo = 0.5 × 2900 √[(1 + 0.3334) / (0.45 + 0.3334) × (1 + 0.3334) / (0.45 + 0.3334)] = 2675.293 mm

Radius of gyration

ix = h/√12 = 400/√12 = 115.47
iz = b/√12 = 300/√12 = 86.602

Slenderness in the x-direction (λx) = 2647.77/115.47 = 22.930
Slenderness in the z-direction (λz) = 2675.293/86.602 = 30.892

Critical Slenderness for the y-direction
λlim = (20.A.B.C)/√n
A = 0.7
B = 1.1
C = 1.7 – M01/M02 = 1.7 – [(-85.832)/175.87] = 2.188
n = NEd / (Ac fcd)
NEd = 716.88 × 103 N
Ac = 400 × 300 = 120000 mm2
fcd = (αcc fck)/1.5 = (0.85 × 30)/1.5 = 17 N/mm2
n = (716.88 × 103) / (120000 × 17) = 0.3514
λlim = (20 × 0.7 × 1.1 × 2.188 )/√0.3514 = 56.842

22.930 < 56.842, second order effects need not to be considered in the y-direction

Critical Slenderness for the z-direction
A = 0.7
B = 1.1
C = 1.7 – M01/M02 = 1.7 – [(-25.269)/35.52] = 2.411
n = NEd / (Ac fcd)
NEd = 716.88 × 103 N
Ac = 400 × 300 = 120000 mm2
fcd = (αcc fck)/1.5 = (0.85 × 30)/1.5 = 17 N/mm2

n = (716.88 × 103) / (120000 × 17) = 0.3514

λlim = (20 × 0.7 × 1.1 × 2.411 )/√0.3514 = 62.634

30.892 < 62.634, second-order effects need not be considered in the z-direction

Design Moments (y-direction)


Y – direction: M01 = 175.87 kNm; M02 = -85.832 kNm

e1 is the geometric imperfection = (θi l0/2) = (1/200) × (2647.77/2) = 6.619 mm

Minimum eccentricity e0 = h/30 = 400/30 = 13.333 mm. Since this is less than 20mm, take minimum eccentricity = 20mm (clause 6.1(4) EC2).

Minimum design moment = e0NEd = 20 × 10-3 × 716.88 = 14.3376 kNm

First order end moment M02 = MTop + eiNEd
eiNEd = 6.619 × 10-3 × 716.88 = 4.745 KNm
M02 = MTop + eiNEd = 175.87 + 4.754 = 180.624 KNm

Longitudinal Steel Area
d2 = Cnom + ϕ/2 + ϕlinks = 40 + 12.5 + 10 = 62.5 mm

d2/h = 62.5/400 = 0.156
Let us read from chart; d2/h = 0.15;

MEd/(fck bh2) = (180.624 × 106)/(30 × 300 × 4002 ) = 0.125
NEd/(fck bh) = (716.88 × 103) / (30 × 300 × 400) = 0.199

COLUMN%2BDESIGN%2BCHART%2Bd2h

From the chart, (As Fyk)/(bhfck) = 0.23

Area of longitudinal steel required As,req = (0.23 × 30 × 400 × 300)/460 = 1800 mm2

As,min = 0.10 NEd/fyd = (0.1 × 716.88)/400 = 0.179 mm2 < 0.002 × 400 × 300 = 240 mm2
As,max = 0.04bh = 4800 mm2

Provide 4Y25mm (Asprov = 1964 mm2)

Design Moments (z-direction)z – direction: M01 = 35.52 kNm; M02 = -25.269 kNm

e1 is the geometric imperfection = (θi l0/2) = (1/200) × (2675.293/2) = 6.688 mm

Minimum eccentricity e0 = h/30 = 400/30 = 13.333 mm. Since this is less than 20mm, take minimum eccentricity = 20mm (clause 6.1(4) EC2)

Minimum design moment = e0NEd = 20 × 10-3 × 716.88 = 14.3376 kNm

First order end moment M02 = MTop + eiNEd
eiNEd = 6.688 × 10-3 × 716.88 = 4.794 KNm
M02 = MTop + eiNEd = 35.52 + 4.794 = 40.314 KNm

Longitudinal Steel Area

d2 = Cnom + ϕ/2 + ϕlinks = 40 + 12.5 + 10 = 62.5 mm
d2/h = 62.5/400 = 0.156

Reading from chart No 1; d2/h = 0.156;
MEd/(fck bh2) = (40.314 × 106)/(30 × 300 × 4002) = 0.0279
NEd/(fck bh) = (716.88 × 103) / (30 × 300 × 400) = 0.199

From the chart, (As Fyk)/(bhfck) = 0.00 (Nominal reinforcement required)

Biaxial Effects

Check if λy / λz ≤ 2.0 and λzy ≤ 2.0

17.203/18.159 = 0.9473 < 2.0, and 18.159/17.203 = 1.0556 < 2.0

Furthermore, let us also check;
(ey/heq) / (ez/beq) ≤ 0.2 or (ez / beq) / (ey / heq) ≤ 0.2

The definition of eccentricity is given in Figure 5.8 of EC2

Definintion%2Bof%2BEccentricity%2BEC2

ey = MEd,y/NEd = (180.624 × 106) / (716.88 × 103) = 251.958 mm
ez = MEd,z/NEd = (40.314 × 106) / (716.88 × 103) = 56.235 mm

heq = iz.√12 = 300 mm
beq = iy.√12 = 400 mm

(ey/heq) ÷ (ez/beq) = 251.958/300 ÷ 56.235/400 = 5.9739 > 0.2

Therefore we have to check for biaxial bending interaction;

(ME,dz/MR,dz )a + (MEd,y/MRd,y )a ≤ 1.0

(As Fyk)/(bhfck) = (1964 × 460) / (30 × 300 × 400) = 0.251

Therefore from the chart; MRd/(fckbh2) = 0.13

MRd = (0.13 × 30 × 300 × 4002) × 10-6 = 187.2 KNm

NRd = Acfcd + Asfyd
NRd = [(300 × 400 × 17) + (1964 × 400)] × 10-3 = 2825.6 kN
NEd/NRd = 716.88 / 2825.6 = 0.2537

To evaluate the value of a, let us look at the table below as given in Clause 5.8.9(4) of EC2

Table%2Bfor%2Ba

By linear interpolation, a = 1.0 + [(0.2537 – 0.1 )/(0.7 – 0.1)] × (1.5 – 1.0) = 1.128

(ME,dz/MR,dz )a + (MEd,y/MRd,y )a ≤ 1.0

(40.314/187.2)1.128 + (180.624/187.2)1.128 = 0.1769 + 0.9606 = 1.1375 > 1.0.
This is not ok, and this shows that 4Y25 is inadequate for the biaxial action on the column.

Let us increase the area of steel to 6Y25mm (Asprov = 2946 mm2)

Let us check again;
(As Fyk)/(bhfck) = (2964 × 460) / (30 × 300 × 400) = 0.3787
Therefore from the chart; MRd/(fckbh2) = 0.175
MRd = (0.175 × 30 × 300 × 4002) × 10-6 = 252 kNm

NRd = Acfcd + Asfyd
NRd = [(300 × 400 × 17) + (2964 × 400)] × 10-3 = 3225.6 kN

NEd/NRd = 716.88 / 3225.6 = 0.222

By linear interpolation, a = 1.0 + [(0.222 – 0.1 )/(0.7 – 0.1)] × (1.5 – 1.0) = 1.102

(ME,dz/MR,dz )a + (MEd,y/MRd,y )a ≤ 1.0

(40.314/252)1.102 + (180.624/252)1.102 = 0.132 + 0.6928 = 0.825 > 1.0.

This shows that 6Y25mm is adequate for the column, and shows some agreement with result from BS 8110-1:1997.

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How to Estimate the Cost of Tiling a 3 Bedrooms Flat

Using tiles to cover the surfaces of floors, walls, countertops, etc can be a very attractive option for finishes in a building. Tiles can provide hard, durable, and aesthetically pleasing surfaces in a building provided that the tiling job is properly done. There are some basic principles that must be followed in order to achieve quality, beautiful and durable tiling.

For a homeowner and/or contractor, cost is a major factor that influences the decision and quality of tiling to be done. The basic factor that can influence the final cost of tiling a house are;

  • Cost of the tiles
  • Cost of screeding
  • Cost of adhesives
  • Cost of grouting cement
  • Cost of tiling accessories such as edge trimmers
  • Cost of labour
  • Size of area to be tiled

In this article, we are going to show how to estimate the cost of tiling a house in Nigeria using a three bedrooms apartment as an example. The floor plan of the three bedrooms apartment is shown in Figure 1. It is desirous to tile all the floors of the building according to the following specifications;

(1) All bedrooms, kitchen, and rear balcony/sit-out: 40cm × 40cm made in Nigeria ceramic tiles

(2) The sitting room, dining, and front balcony/sit-out: (30cm × 60cm) imported Virony glazed tiles;

(3) All the toilets and bathrooms: (30cm × 30cm) made in Nigeria ceramic tiles.

We are required to estimate the total cost of tiling the entire floor of the building, considering materials and labour.

FLOOR%2BPLAN
Figure 1: Floor plan of a three bedrooms apartment

Material Prices (informative)

It is very important for you to make an adequate market survey, in order to know the exact prices of materials in your area. This is the only chance you have of making a reasonably accurate estimate. The prices stated below are a bit representative, but merely informative. Note that tiles with designs may be more expensive than plain tiles or tiles with a single colour.

(40cm × 40cm) Ceramics Tiles = ₦3,360 per carton (12 pieces per carton – 1.92 square metre)

(30cm × 60cm) Porcelain Glazed Tiles = ₦5,760 per carton (8 pieces per carton – 1.44 square metre)

(30cm × 30cm) Ceramic Tiles = ₦2,700 per carton (17 pieces per carton – 1.53 square metre)

1 tonne of sand = ₦4,000

1 bag of cement = ₦4,000
5 kg of white cement = ₦2,500
Water seal = ₦700 per kg
Tile gum (20kg) = ₦1,450

BILL NO 1: TILES AND TILING ACCESSORIES
(a) Tiling of the bedrooms, kitchen, backyard sit-out, and store with (40cm × 40cm) Time Ceramics Tiles

We have to calculate the floor areas where we are going to apply the (40cm × 40cm) tiles;

Bedroom 1 = (3.6m × 3.45m) = 12.42 m2
Bedroom 2 = (3.6m × 3.6m) = 12.96 m2
Bedroom 3 = (3.15m × 3.17m) = 9.9855 m2
Kitchen = [(3.35m × 2.35m) + (1.37m × 1.075m)] = 9.34525 m2
Store = (2.025m × 1.775m) = 3.59 m2
Kitchen Sit-out = (1.37m × 2.075m) = 2.84275 m2
Total Area  = 51.148 m2

Area of a piece of tile = (0.4m × 0.4m) = 0.16 m2

The number of pieces of tiles required to complete the floor areas = 51.148/0.16 = 319.675 pcs

Therefore, the number of cartons required = 319.675/12 = 26.639 cartons.

We will therefore provide 30 cartons of (40cm × 40cm) ceramic tiles. Extra tiles will account for damages, and for skirting of the foot of the walls.

Therefore the cost of the (40cm x 40cm) tiles   = 30 × ₦3,360 = ₦100,800

(b) Tiling of the sitting room, dining, and entrance porch with (60cm x 30cm) tiles

The floor areas where we are going to apply the (60cm × 30cm) tiles;

Sitting room = (5.65m × 4.625m) = 26.13125 m2
Dining = (2.35m × 3.35m) = 7.8725 m2
Entrance Porch = (3.78m × 1.475m) = 5.5755 m2
Total Area  = 39.579 m2

Area of a piece of tile = (0.6m × 0.3m) = 0.18 m2

The number of pieces of tiles required to complete the floor areas = 39.579/0.18 = 219.883 pcs;

Therefore, the number of cartons required = 219.883/8 = 27.485 cartons

We will therefore also provide 30 cartons of (60cm × 30cm) ceramic tiles.

Therefore the cost of the (60cm x 30cm) tiles = 30 × ₦5,760 = ₦172,800

(c) Tiling of the bathroom and toilet floors with (30cm x 30cm) tiles

On calculating the floor areas where we going to apply the (30cm × 30cm) tiles;

Bathroom and Toilet 1 and 2 = 2(2.0m × 1.1m) = 4.4 m2
Bathroom and toilet 3 = (2.0m × 0.985m) = 1.97 m2
Visitor’s toilet = (2.0m × 0.875m) = 1.75 m2
Total Area  = 8.12 m2

Area of a piece of tile = (0.3m × 0.3m) = 0.09 m2

The number of pieces of tiles required to complete the floor areas = 8.12/0.09 = 90.222 pcs

Therefore, the number of cartons required = 90.222/17 = 5.307 cartons

We will therefore provide 7 cartons of (30cm × 30cm) ceramic tiles

Therefore the cost of the (30cm x 30cm) tiles = 7 × ₦2,700 = ₦18,900


(d) Loading, transportation, and offloading at the site (say)  = ₦20,000


Therefore, sub-total 1 = ₦100,800 + ₦172,800 + ₦18,900 + ₦20,000 = ₦312,500


BILL NO 2: CEMENT AND SAND
We are going to make 25mm thick screeding to receive the tiles.

From above, you can verify that the total floor area of the building = 51.148 m2   39.579 m2    8.12 m2  =  98.847 m2

Volume of mortar required = 98.847 × 0.025 = 2.471 m3
Using a mix ratio of 1:5

Cement required = 6 bags/m3
Sand required = 1800 kg/m3

Cement required = 14.826 bags (provide 15 bags)
Sand required = 4.447 tonnes (provide 5 tonnes)


Alternative calculation by site experience
From experience, 2 bags of cement is sufficient to complete the entire tiling process of (3.6m × 3.6m) room

Therefore;
2 bags of cement = 12.96 m2
x bags of cement = 98.847 m2

On solving;
x = 15.254 bags of cement; say 16 bags of cement


From experience, about 20 – 22 head pans of sharp sand is sufficient to complete the entire screeding process of (3.6m × 3.6m) room;

22 head pans = 22 × 0.0175 m= 0.385 m3

Therefore;
0.385 m3 of sand = 12.96 m2
x m3 of sand = 98.847 m2

On solving; 

x2.936 m3 sand = 4.844 tonnes of sand

Therefore, provide
;

5 tonnes of sharp sand = ₦20,000
The cost of cement = 16 × ₦4,000 = ₦64,600
Water seal = 16 packs = 16 × ₦700 = ₦11,200
Tile gum = 17 bags × ₦1450 = ₦24,650
Other tiling accessories (allow) = ₦20,000
Transportation (say) = ₦5,000

Sub total 2 = ₦145,450

BILL NO 3: LABOUR

Cost of tiling  1mof floor = ₦500

Therefore;
1 m2 = ₦350
98.847 m2 = x

On solving; 

x = ₦49,423 (rounding up to the nearest 100)

Therefore, cost of labour = ₦50,000


GRAND TOTAL =  ₦ 312,500  +  ₦145,450  +  ₦50,000  = ₦507,950

Therefore the cost of tiling the floor of the building = ₦507,950 + VAT + Engineer’s/Architect’s Profits

Thank you for reading

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