Slab System

35
Chapter 1 : Slab system Our slabs are designed as partially prestressed , that is 80% of self weight is designed as Post-tensioned flat slab and the remaining portions are designed as reinforced concrete . A-Slab thickness From table 9.5 (c) , the slab thickness chosen is l 33 = 303.3 mm . Thus , use 350 mm slab thickness : B- Load calculations :

description

slab desin

Transcript of Slab System

Page 1: Slab System

Chapter 1 : Slab system

Our slabs are designed as partially prestressed , that is 80% of self weight is designed as Post-tensioned flat slab and the remaining portions are designed as reinforced concrete.

A-Slab thickness

From table 9.5 (c) , the slab thickness chosen is l33 = 303.3 mm.

Thus , use 350 mm slab thickness :

B- Load calculations: 1.Dead load:

Plastering = 1510 * 21 = 31.5 Kg

Sand = 1 * 0.125 * 1800 = 225 KgMortar = 1 * 0.03 * 2100 = 63 Kg

Tile = 2010 * 20 = 40 Kg

Total DL = 360 Kg / m2 = 3.56 KN/m2

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2 .Live Load: From the ACSE , the Live load is determined referring to the occupancy category of the building ( residential building ).

From the figure ; the LL is 4.79 KN¿m2

The next step is to start the design of our slabs using csi SAFE , however ; the self load multiplier of the slab own weight is set to be 0.2 since 0.8 of the slab weight will be carried by the Strands of post-tensioning , we'll start our

design by designing the slab as reinforced concrete:

1. Defining the materials , sections , spans , design strips , loads and load combinations .

The following figures will illustrates how to input the design info. Starting from the materials until being ready for running analysis and design.

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The above figure illustrates splitting the Slab into design strips of width equal 10 m , this design strip is composed of a column strip of width 5 m , and two half middle strips with 2.5 width each.

Actually ; using the ACI Direct Design Method is not permitted here since the loads includes Non-gravity load ( earthquake loads and wind loads ) , however ; the csi SAFE will use a more accurate procedures of design , which is the Equivalent frame method.

Now defining the loads as follows :

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Now after adding the loads , csi SAFE will automatically set the Design combinations and the design will be according to the

controlled one as showing in the figures below:

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2- Design and analysis Results .

Now we are ready to the run the analysis and design of the slabs

Hint : moving the cursor at any point will give the value of the moment at that point ( eg. Max. moment is 445.4 KN/m

2).

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As mentioned above , csi SAFE enable us to select the bar size that we will use in the slabs : the following figures will

illustrates the complete design of the strips:

Note : the blue line indicates the limit for the minimum reinforcement ; i.e : most slabs will require only minimum reinforcement except the exterior spans , that’s because a large quantity of the load is held by the STRANDS ( 80 % of self

weight )!!!!!!

In the N-S Direction:

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In The E-W Direction:

Note here the top steel will require a design rather than minimum reinforcement :

Moving the cursor across the diagram ( reinforcement diagram ) will give the required amount of bars , that’s enable us easily for applying bar cut-off for more economic design.

Requirement of placing steel bars:

While applying cut off of bars in two way slabs , some bars must remain constant across the strips and must not be cut , the ACI

code showed this thing and recommended the following :

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These figures is clear enough for applying cut-off providing that the requirement of the Development length is satisfied.

Summary of Reinforcement :

Provide minimum reinforcement bottom steel in the Design strips , That is ρmin=0 .0018 Ag uniformly distributed across the bay width , also provide the required amount of top steel as suggested by csi SAFE uniformly distributed over the effective

band with of the support.

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Manual Design of post-tensioned concrete slab to balance 80% of self weight of the slab.

MATERIALS:

-f'c = 35 Mpa-ɣ for concrete = 24 KN/m.s

-fci'= 0.75f'c= 27 Mpa-fpu= 1860 Mpa , fps not exceeding 1276 Mpa

-fpy = 1690 Mpa-fpe = 1100 Mpa-Eps = 200 Gpa

-fy = 420 Mpa -Stress-relived strands ( K 270 )

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-Slab thickness = 350 mm. -Unsupported length of the column ( story height ) = 4 m

-ft = 0.25√ f ' c = 1.48 Mpa. -fc = 0.45 f'c = 15.8 Mpa.

-Self weight = 24 * 0.35 = 8.4 KN/m.s-Balance ratio = 0.8 →0.8 * 8.4 = 6.72 KN/m.s

The analysis here is based on the Equivalent-frame method as recommended by the ACI Code:

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As shown in the figure , the analysis here is based on an

equivalent frame taken in the N-S direction , since all spans

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are same in magnitudes , also all columns are equal in dimension , analysis for one equivalent frame is enough for finding the required # of strands and non-bonded reinforcement for the whole slabs in the both directions.

Hmin= L / 30 = 10000/30 = 333.33 mm →Use h = 350 mm .Ww = 6.72 KN/m.sWu = 1.2 * 6.72 = 8.06 KN/m.s

→assume an average intensity of compressive stress due to balancing is fc = 1.17 Mpa , then unit F = 1.17 *350*1000 =

409.5 KN/m , so ; trying 12in diameter seven wires stress relived

strands ; Pe = Aps * fpe = 99*1100 = 108.9 KN , for L = 10 m ,

total Fe = 409.5 * 10 = 4095 KN .# of strands per bay is FePe =

4095/108.9 = 37 strands , and total Pe = Fe = 108.9 * 37 = 4029.3 KN , the actual unit force F = 4029.3/10 = 402.93 KN/m

, and the actual unit stress is fc = 402.9∗103

1000∗350 = 1.15 Mpa < 1.17

Mpa , which is satisfactory . Consequently , use fc = 1.15 Mpa due to load balancing , and assume a tendon profile as shown in

the figure below :

-a1 = 175+300

2 - 50 = 187.5 mm , a2 = 350 – 50 – 100 = 200 mm.

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Wbal = 8F a

l2 =

8∗402.93∗0.1875102

= 6.044 KN/m.s

Wnet = 6.72 – 6.044 = 0.676 KN/m.s for the exterior span.

Wbal = 8F a

l2 =

8∗402.93∗0.2102

= 6.45 KN/m.s

Wnet = 6.72 – 6.45 = 0.27 KN/m.s for the interior span.

Equivalent frame characteristic

Kc = 4 I c Ec

l−2h =

4∗Ec∗400∗4003∗112

4000−(2∗350 ) = 2585858.586 Ec

C = ∑ (¿1−0.63 xy)( x3 y3 )¿

) = 1 -0.63 * 350400 ) * ( 3503∗400

3¿ =2565354167 mm4

Kt = ∑ 9C Ecs

l 2(1− c2l 2

)3 =

9∗2565354167∗Ecs

10,000∗(1− 40010000

)3 +

9∗2565354167∗Ecs

10,000∗(1− 40010000

)3

= 5219226.414Ecs

Kec = 1

1kc

+1k t

= 1

12585858.586

+1

5219226.414 = 1729152.367 Ecs

Ks = 4 I c Ecs

ln−C1

2 =

4∗10000∗3503∗Ecs

12∗(10000−4002 ) = 14583333.33 Ecs

Since all members are of the same concrete material , Ec cancels each other.

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Exterior column :

DF = Ks

∑ K

=Ks

Kec+Ks ¿+Ks¿=

14583333.33

14583333.33+1729152.367 = 0.894

Interior columns:

DF = Ks

∑ K=

Ks

Kec+Ks ¿+Ks¿=

14583333.33

14583333.33+14583333.33+1729152.367 = 0.472

EXT. Span : FEM = w l2

12 = 0.676∗10

2

12 = 5.633 KN.m

Int . Span : FEM = w l2

12 = 0.27∗10

2

12 = 2.25 KN.m

DCBAPointDC DE

CB CD

BA BC

ABMember

0.47 0.470.47 0.470.47 0.470.894DF+2.25- 2.25

0 0+2.25- 2.25

0 0+5.6-

2.25-1.6- 1.6

-5.64.98

FEMDist.

-0.70.37 0.37

+ 2.5 0 -1.17- 0.95

-0.790.71

CODist.

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5.36- 5.01

-0.734Final Mnet

Mnet = 5.36 KN.m

Slab concrete tensile stress at support.

Maximum Mnet = 5.36 – ( 0.27∗102 *

0.43 ) = 5.18 KN.m

Slab section modulus , S = b h2

6 = 10000∗350

2

6 = 204166666.7mm3.

Ftop = −P

A + MS = -1.15 +

5.18∗106

204166666.67 = -1.13 Mpa , OK.

Slab concrete tensile stress at Midspan.

Maximum Mnet = 0.27∗102

8 - 5.36 = -1.805 KN.m

Ftop = -1.15 + −1.805∗106

204166666.67 = -1.158 Mpa , OK .

Ultimate flexural strength analysis

1. Balanced Moment

-Exterior span :

FEMbal=W b l2

12 = 6.044∗102

12 = 50.4 KN.m

-Interior span:

FEMbal=W b l2

12 = 6.45∗102

12 = 53.8 KN.m

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Now Running a moment distribution will determine the maximum balanced moment for the exterior column joints.

DCBAPointDC DE

CB CD

BA BC

ABMember

0.47 0.470.47 0.470.47 0.470.894DF+53.8- 53.8

0 0+53.8- 53.8

0 050.4-

53.8+1.6- 1.6

-50.444.8

FEMDist.

-0.80.37 0.37

22.4 0 -10.5- 10.5

0.80.71-

CODist.

63.9- 65.9

-5.46Final Mnet

2. Secondary Moments ( Ms ) and factored load moment ( Mu )

-Exterior span :

From tendon profile , e = 0.0 mm.

M1 = Primary moment = Pe.e = 0.0 KN.m

M bal- = 5.46 KN.m

Ms = M bal - M1 = -5.46 KN.m

Factored FEM = W u l2

12 = 8.064∗10

2

12 = 67.2 KN.m

-Interior span :

From tendon profile , e = 175-50 = 125 mm

M1 = Pe . e = 402.93 * 125 = 50.4 KN.m

M bal = 63.9 KN.m

Ms = 50.4 – 63.9 = 13.5 KN.m

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Factored FEM = 67.2 KN.m

And now running a moment distribution for the factored moments , here analysis of pattern loading should be made to determine the worst case of the service and factored loads.

DCBAPointDC DE

CB CD

BA BC

ABMember

0.47 0.470.47 0.470.47 0.470.894DF+67.2- 67.2

0 067.2-

67.20 0

-67.259.81

FEMDist.

-0.80.37 0.37

29.9-14.1- 14.1

00

CODist.

82.2- 81.3

-5.46Final Mnet

3. Design Moments Mu

The design moments are the difference between the factored load moments and the secondary moments.

Exterior span:

Mu = 7.4 – 5.46 = 1.94 KN.m

Interior span BA :

Mu = 82.2 -13.5 = 68.7 KN.m

Interior span BC :

Mu = 81.3 – 15.5 = 65.8 KN.m

Moment reduction to the column face of support = V . c3

V = W u .l

2 -

∆ Mln

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For the exterior span :

V = 8.064∗10

2 – 82.2−7.410 = 32.84 KN.m

V . c3

= 32.84∗0.42

= 4.4 KN.m

Centerline moment = 6.6 – 1.94 = 2.5 KN.m

Required Mn = Mu∅ =

4.70.9 = 5.2 KN.m

For the interior span BA:

V = 8.064∗10

2 – 7.4−82.210 = 47.8 KN.m

V . c3

= 47.8∗0.43

= 6.4 KN.m

Mu = 68.7 – 6.4 = 62.3 KN.m

Required Mn = Mu∅ =

62.30.9 = 69.2 KN.m

For the interior span BC:

Since the factored moment is almost the same →the required moment is smaller than the previous span , thus ignore it.

Span AB maximum positive moment

Assume point of zero shear ( or max. moment ) is at ( X ) m from face A :

X = V AB

W AB =

32.848.064 = 4.07 m

Maximum positive moment = V AB . x−W u x2

2−M u+M s

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=4.07*32.84−8.06∗4.072

2−¿ 7.4 + 5.46

=64.93 KN.m

Required M n=M u

∅ = 64.930.9 = 72.14 KN.m

Span AB maximum positive moment

Unadjusted Max. +ve moment = W u .l2

8 = 8.064∗10

2

8 = 100.1 KN.m

+ve Moment = 100.1 – 82.2 + 15.5 = 33.4 KN.m

3 . Flexural strength ( Nominal moment strength )

1-Interior supports ( top face of the support )

As required by the ACI Code :

As = 0.00075 Acf

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= 0.00075 * 350 * 1000 = 262.5 mm2

Thus use 5 ∅ 10 → As provided = 71*5 = 355 mm2

Spacing = 1000– (5∗10)

4 = 238 mm ≤ 300 mm , Ok.

ρp = A ps

bd =

36∗9910000∗300 = 0.0014

f pe = 1100 Mpa.

f ps =f pe + 70 + f c

'

100 ρp

= 100 + 70 + 35

100∗.0012 = 1462 Mpa.

F ps = 1462∗99∗36

10 = 521.1 KN per meter width of the slab.

F s = 420 * 355 = 149.1 KN per meter width of the slab.

Now , the total force provided by both reinforcement types

( bonded and non bonded ) is:

F t = 521.1 + 149.1 = 670.2 KN.

a=A s . f y+ Aps . f ps

0.85 f c' b

= 670.2∗103

0.85∗35∗1000 = 22.53 mm

ad p

= 22.53300

= 0.08 < 0.319 → T.C , Ok

.

M n=( A s . f y+ Aps . f ps )(d−a2 )

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= 670.2 ) * 300 – 22.532 = ( 193.5 KN.m < 69.2 KN.m , Ok.

2- Mid-span section ( +ve moment )

F ps = 521.1 KN

a= 521.1∗103

0.85∗35∗1000 =17.5 mm

ad

< 0.319 , Ok ,,,,, TC!

M n=521.1∗(300−17.52 )=136.6KN >72.14KN .m

Summary :

Use 37 Strands uniformly distributed across the bay width with 5 ∅ 10 at the top fiber at the support section .

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