For long span slabs in a building subjected to light load, ribbed slabs are more economical than solid slabs. In ribbed slab construction, reduction in volume of concrete is achieved by removing some of the concrete below the neutral axis of the section, under the assumption that the tensile strength of concrete is negligible. Two major forms of construction of ribbed slab are;

(1) Ribbed slab without permanent blocks

(2) Ribbed slab with permanent blocks

The major advantage of ribbed slab with permanent blocks is the reduction in the quantity of formwork required, given the fact that strength of the blocks is normally not assumed to contribute to the strength of the slab in design. In Nigeria, clay hollow pot and sandcrete blocks have been successfully used, but on the rise is the polystyrene. Polystyrene offers the advantage of light weight, improved fire resistance, and economy, at the expense of less rigidity compared to clay hollow pot or blocks.

Fig 2: Expanded Polystyrene (EPS) |

In this post, we are going to consider the design of a floor (see figure 2) subjected to the following loading conditions;

Fig 3: Preliminary Structural Arrangement |

^{2}

Partition allowance - 1.5 kN/m

^{2}

Imposed load - 2.5 kN/m

^{2}

f

_{ck}= 30 Mpa, f

_{yk}= 500 Mpa, Concrete cover = 25 mm

The structural engineer decided the scheme the structure as shown in figure 4. The slab is made thick close to the supports, to enable adequate transmission of shear forces.

Fig 4: Adopted Structural Scheme |

From basic span/effective depth ratio of 26, let us choose a trial depth;

6000/26 = 231 mm

Let us try a total depth of 250 mm

Fig 5: Transverse Section Through The Slab |

Fig 6: Longitudinal Section Through the Slab |

**Load Analysis**

For 500mm c/c rib spacing;

*Permanent Actions*Weight of topping: 0.075 × 25 × 0.5 = 0.9375 kN/m

Weight of ribs: 0.15 × 0.175 × 25 = 0.656 kN/m

Weight of finishes: 1.2 × 0.5 = 0.6 kN/m

Partition allowance: 1.5 × 0.5 = 0.75 kN/m

Weight of heavy duty EPS (16 kg/m3) = 0.156 × 0.175 × 0.5 = 0.01365 kN/m

Total dead load g

_{k}= 2.95 kN/m

*Variables Action(s)*Occupancy load q

_{k}: 2.5 × 0.5 = 1.25 kN/m

At ultimate limit state; 1.35g

_{k}+ 1.5q

_{k}= 1.35(2.95) + 1.5(1.25) = 5.8575 kN/m

**Structural Analysis**

The design load per span at ultimate limit state (F) is given by = 5.8575 kN/m × 6m = 35.145 kN/m

From clause 3.5.2.3 of BS 8110-1:1997, we can use the simplified method for structural analysis.

At the middle of span 1-2; M = 0.075 × 35.145 × 6 = 15.815 kNm

At support 2, M

_{Ed}= -0.086 × 35.145 × 6 = 18.134 kNm

**Designing the span as a T-beam;**

M

_{Ed}= 15.815 kN.m

Effective depth (d) = h – C

_{nom}– ϕ/2 - ϕ

_{links}

Assuming ϕ12 mm bars will be employed for the main bars, and ϕ10 mm bars for the stirrups (links)

d = 250 - 25 - (12/2) -10 = 209 mm

k = M

_{Ed}/(f

_{ck}bd

^{2}) = (15.815 × 10

^{6})/(30 × 500 × 209

^{2}) = 0.024

Since k < 0.167, no compression reinforcement required

z = d[0.5+ √(0.25 - 0.882k)]

k’ = 0.024

z = d[0.5+ √((0.25 - 0.882(0.024))] = 0.95d = 198.55 mm

Depth to neutral axis x = 2.5(d - z) = 2.5(209 - 198.55) = 26.125 mm < 1.25hf (93.75mm)

Therefore, we design rib as a rectangular section

Area of tension reinforcement A

_{s1}= M

_{Ed}/ (0.87f

_{yk}z)

A

_{s1}= M

_{Ed}/ (0.87f

_{yk}z) = (15.815 × 10

^{6}) / (0.87 × 500 × 0.95 × 209) = 183 mm

^{2}

Provide 2H12 Bot (A

_{Sprov}= 226 mm

^{2})

**Check for deflection**

ρ = A

_{s,req}/bd = 183 / (500 × 209) = 0.00175

ρ

_{0}= reference reinforcement ratio = 10

^{-3}√(f

_{ck}) = 10

^{-3}√(30) = 0.00547

Since ρ ≤ ρ

_{0};

L/d = k [11 + 1.5√(f

_{ck}) ρ

_{0}/ρ + 3.2√(f

_{ck}) (ρ

_{0}/ ρ - 1)

^{(3⁄2)}]

k = 1.3

L/d = 1.3 [11 + 1.5√(30) × (0.00547/0.00175) + 3.2√(30) × [(0.00547 / 0.00175) - 1]

^{(3⁄2)}]

L/d = 1.3[11 + 25.68 + 54.321] = 118.3

β

_{s}= (500 As

_{prov})/(f

_{yk}As

_{req}) = (500 × 226) / (500 × 183) = 1.23

beff/bw = 500/150 = 3.33

Therefore multiply basic length/effective depth ratio by 0.8

Therefore limiting L/d = 1.23 × 0.8 × 118.3 = 116.41

Actual L/d = 6000/209 = 28.708

Since Actual L/d (28.708) < Limiting L/d (116.41), deflection is satisfactory.

**Design of Support 2;**

M

_{Ed}= 18.134 kN.m

Effective depth (d) = h – C

_{nom}– ϕ/2 - ϕ

_{links}

Assuming ϕ12 mm bars will be employed for the main bars, and ϕ10 mm bars for the stirrups (links)

d = 250 - 25 - (12/2) -10 = 209 mm

k = M

_{Ed}/(f

_{ck}bd

^{2}) = (18.134 × 10

^{6})/(30 × 150 × 209

^{2}) = 0.0922

Since k < 0.167, no compression reinforcement required

z = d[0.5+ √(0.25 - 0.882k)]

k = 0.092

z = d[0.5+ √((0.25 - 0.882(0.092))] = 0.91d

Area of tension reinforcement A

_{s1}= M

_{Ed}/ (0.87f

_{yk}z)

A

_{s1}= M

_{Ed}/ (0.87f

_{yk}z) = (18.134 × 10

^{6}) / (0.87 × 500 × 0.91 × 209) = 219 mm

^{2}

Provide 2H12 Top (A

_{Sprov}= 226 mm

^{2})

**Shear Design**

**Maximum shear force in the rib**V

_{Ed}= 0.6F = 0.6 × 35.145 = 21.087 kN

V

_{Rd,c}= [C

_{Rd,c}.k.(100ρ

_{1}f

_{ck})

^{(1/3)}+ k

_{1}.σ

_{cp}]b

_{w}.d ≥ (V

_{min}+ k

_{1}.σ

_{cp}) b

_{w}.d

C

_{Rd,c}= 0.18/γ

_{c}= 0.18/1.5 = 0.12

k = 1 + √(200/d) = 1 + √(200/209) = 1.97 < 2.0, therefore, k = 1.97

V

_{min}= 0.035k

^{(3/2)}f

_{ck}

^{0.5}

V

_{min}= 0.035 × (1.97)

^{1.5}× 30

^{0.5}= 0.53 N/mm

^{2}

ρ

_{1}= As/bd = 226/(150 × 209) = 0.0072 < 0.02; Therefore take 0.0072

V

_{Rd,c}= [0.12 × 1.97 (100 × 0.0072 × 30 )

^{(1/3)}] × 150 × 209 = 20639.67 N = 20.639 kN

Since V

_{Rd,c}(20.639 kN) < V

_{Ed}(21.087 kN), shear reinforcement is required.

The compression capacity of the compression strut (V

_{Rd,max}) assuming θ = 21.8° (cot θ = 2.5)

V

_{Rd,max}= (b

_{w}.z.v

_{1}.f

_{cd}) / (cotθ + tanθ)

V

_{1}= 0.6(1 - f

_{ck}/250) = 0.6(1 - 30/250) = 0.528

f

_{cd}= (α

_{cc}f

_{ck}) / γ

_{c}= (0.85 × 30) / 1.5 = 17 N/mm

^{2}

Let z = 0.9d

V

_{Rd,max }= [(150 × 0.9 × 209 × 0.528 × 17) / (2.5 + 0.4)] × 10

^{-3}= 87.333 kN

Since < V

_{Ed}< V

_{Rd,c}< V

_{Rd,max}

_{}Hence A

_{sw}/ S = V

_{Ed}/ (0.87 F

_{yk}z cot θ) = 21087 / (0.87 × 500 × 0.9 × 209 × 2.5 ) = 0.103

**Minimum shear reinforcement;**

A

_{sw}/ S = ρ

_{w,min}× b

_{w}× sinα (α = 90° for vertical links)

ρ

_{w,min}= (0.08 × √(f

_{ck})) / f

_{yk}= (0.08 × √30) / 500 = 0.000876

A

_{sw}/S

_{min}= 0.000876 × 150 × 1 = 0.131

Maximum spacing of shear links = 0.75d = 0.75 × 209 = 156.75 mm

Provide H8mm @ 150 mm c/c as shear links.

**Slab Topping**

A142 BRC Mesh can be provided or H8 @ 250mm c/c

For more information on design and consultancy to accomplish the most challenging design brief, contact the author on info@structville.com. Thank you, and God bless you.

Weldone bro

ReplyDeleteThank you very much.

DeleteGood work here Engr..

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