13 (seismic) lateral loads effects (eng a farghal)

Page 1

( Lateral Loads ) Seismic &Wind

By: Eng. Ahmed Farghal. Table of Contents. Introduction. Equivalent static load method. Steps of Calculating Seismic Load. Wind Loads. Systems resisting lateral loads. Design of Shear wall. Drift of structures due to seismic loads Examples.

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Page No.

2 12 25 37 48 57 66 70


Lateral Loads Introduction. 1- Seismic loads. 2- Wind loads.

1. Seismic Loads: (

)

Seismic sources 1- Movements of tectonic plates 2- Movements of faults 3- Volcanoes 4- Failure of roof of large cave 5- Mankind effect (explosion, fill and in-fill of dams ..... etc.) 6- Undefined reasons C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


Types of surface waves Love wave Rayleigh wave

Love wave Di

re c

Pa rti

cle

Rayleigh wave tio

Di no

re c

fp rop ag ati on

Pa rti

mo tio n

cle

tio

no

mo tio n

Classification of earthquakes 1- Deep focus earthquakes Focal depth > 300 km

Epicentral distance Epicenter

2- Intermediate focus earthquakes 300 km > Focal depth > 70 km

Focal depth

3- Shallow focus earthquakes Focal depth < 70 km

l tra n ce nce o yp ta H dis

Focus or Hypocenter

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fp rop ag ati on


Methods of measuring earthquakes magnitude The Richter Scale - The magnitude of most earthquakes is measured on richter scale. - It was invented by Charles F. Richter in 1934. - The richter magnitude is calculated from the amplitude of the largest seismic wave recorded for the earthquake, no matter what type of wave was the strongest.

The Mercalli Scale - It is another way to measure the strength of an earthquake. - It was invented by Giuseppe Mercalli in 1902. - This scale uses the observations of the people who experienced the earthquake to estimate its intensity.

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Methods of analysis of structures under seismic load

1- Equivalent Static Load (Simplified Modal Response Spectrum).

2- Multi-Modal Response Spectrum Method.

3- Time History Analysis.

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1- Equivalent Static Load (Simplified Modal Response Spectrum).

Fundamental period (T1) T1 < 4 T C where: TC =

1 H

and

T1 < 2.0 Seconds

Response Spectrum Curve

60 m

H = H

2

L B

4.0

B

L = B=

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H

)

Page No.

L


3 Uniform shape

4 Uniform statical system

Sec 4 Sec 3 Sec 2

H

Sec 1 Core

Sec 2 Shear wall

Sec 3 Solid Slab

Sec 4 Flat Slab

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Sec 1

Page No.


(Lx / L y ) (e o ) (x , y e > 0.15 L

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L2 L1

H L3

L1 L

L1 - L 2 < 0.20 L1

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> 0.15 H

L1 + L 3 < 0.20 L

)

Page No.


L2 L1

H L3

L1 L

L

< 0.15 H

L 1+ L3 < 0.50 L

L - L2 < 0.30 L L1 - L 2 < 0.10 L1

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2- Multi-Modal Response Spectrum Method

Sd (T)

Response Spectrum Curve

Time (Sec)

( Rotation

Response Spectrum Curve Displacement

3- Time History Analysis.

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Equivalent static load method: (Simplified Modal Response Spectrum Method) Z

Fb

Fb

1

L

B

Side View

Y

1

L

Plan

Fb

X

re Mo tical Cri

B

Elevation Fb

2

( More Critical ) 2

X ,Y Manual More Critical

Y

X

0.3 E Fx

E Fx E Fy

0.3 E Fy

ET = 0.3 E Fx + E Fy C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

ET = E Fx + 0.3 E Fy )

Page No.


+

Fb = Sd (T1)

l W g

where: Fb = Ultimate base shear force = Gravitational acceleration g Sd (T1) = Response Spectrum

(T1)

Sd (T) 2.5 ag S g1

Response Spectrum Curve

ag S g1 Sd (T) 1

TB TC

T1

( Rotation

TD

4.0

Time (Sec)

Response Spectrum Curve Displacement

Response Spectrum 0 < T < TB

2.5 h - 2 ) : Sd (T) = a g g1 S 32 + T ( TB R 3

TB < T < TC

h : Sd (T) = a g g1 S 2.5 R

TC < T < TD

: Sd (T) = a g g1 S 2.5 R

TC h > 0.20 a g g1 T

TC TD h TD < T < 4.0 Sec : Sd (T) = a g g1 S 2.5 > R T2 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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0.20 ag g1

Page No.


where:

T

= Periodic time of different mode shapes (Different mode shapes) TB,TC ,TD , S , a g

ag =

Zone

Design acceleration

Zone 1 Zone 2 Zone 3 Zone 4 Zone 5A Zone 5B

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(a g ) 0.10 g 0.125 g 0.15 g 0.20 g 0.25 g 0.30 g

)

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26

28

T ER S E TD

27

29

Dakhla Oasis

Bahariya Oasis

30

31

Kharga Oasis

Asyut

El Minya

32

Sohag

Beni Suef

Cairo Giza

Ismailia

Damietta

32

33

Kosetta Port Said Damanhur El Mansura Tanta

Al Fayum

Bahariya

Alamein

Alexandria

31

33

Aswan

35

Ras Muhammad

Quseir

Safaga

Hurghada

34

Kom Ombo

Idfu

Luxor

Qena

El Arish

34

36

Page No.

35

36

22 37

23

24

25

26

27

28

29

30

31

37 32

Halaib

Ras Banas

Marsa Alam

RT E ES D T

22 25

S WE

23

30

S EA

24

25

Siwe

Matruh

29

MEDITERRIAN SEA

28

EZ SU

26

27

28

29

30

31

Salum

27

G

26 2

) ces/ mc( AGP

25 32

L FLU

GU F FO AF O

AI AB A U

S IN EA S D RE

250

200

150

125

100

50

Zone 5B

Zone 5A

Zone 4

Zone 3

Zone 2

Zone 1


T B ,TC ,TD , S

TB ,TC = elastic response spectrum TD = spectrum S = Soil Factor

Subsoil Soil Class Type

A

Rock

B

Dense Soil

Soil Description

Meduim Soil

C

D

Loose Soil

For Type (1) Subsoil Class A B C D

S 1.00 1.35 1.50 1.80

TB 0.05 0.05 0.10 0.10

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TC 0.25 0.25 0.25 0.30 )

TD 1.20 1.20 1.20 1.20 Page No.


For Type (2) Subsoil Class A B C D

g1 =

S 1.00 1.20 1.25 1.35

TB 0.15 0.15 0.20 0.20

TC 0.40 0.50 0.60 0.80

TD 2.00 2.00 2.00 2.00

Importance factor

Importance

Category

Type of Structures

Importance Factor (g1)

I

1.40

II

1.20

III

1.00

IV

0.80

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R = Response modification factor R :

4.50 3.50 2.00

:

5.00 4.50 4.50

: 7.00 5.00

6.00 5.00

:

:

3.00 3.50 5.00

Response modification factor (R)

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3.00 3.50

6.00 5.00

7.00 5.00

5.00 4.50 4.50

4.50 3.50 2.00

R

5.00

:

:

:

Response modification factor (R)

:

:

R = Response modification factor

+ R.C. Shear Walls or Cores

Frames with Bracing OR

R = 5.0

R = 4.5

Non Ductile Frames R = 5.0

Ductile Frames R = 6.0

Non Ductile Frames R = 5.0

Ductile Frames R = 7.0

NO R.C. Shear Walls or Cores or Bracing

R.C. Shear Walls or Cores

Frames with Bracing

R


h=

Damping factor corrected for horizontal response spectrum Type of Structure Steel with Welded Connections Steel with Bolted Connections Reinforced Concrete Prestressed Concrete Reinforced Masonry Walls 1.00

h 1.20 1.05 1.00 1.05 0.95

Damping factor (h)

Prestressed Concrete

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Response Spectrum

+

Fb = Sd (T1)

Fb

l W g

where: Fb = Ultimate base shear force = Gravitational acceleration g Sd (T1) = Response Spectrum

(T1)

T1 = Fundamental period of the building T1 = Ct H

3/4

where: H = Height of the building from foundation level

H

Ct = Factor depend on structural system and material Structural System Steel moment resisting frames Reinforced concrete moment resisting frames (Space frames) Ductile frames (beams & columns) Non-ductile frames (flat slabs) All other buildings Cores or Shear walls Combinations of (cores or shear walls) & frames C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Ct 0.085 0.075

0.050

Page No.


Shear wall + Core ( Ct = 0.05)

Frames + Shear wall (C t = 0.05)

Non-ductile frames (Flat Slab) ( C t = 0.075)

Ductile frames (Beams + Slab) ( C t = 0.075)

T1

Range

Response Spectrum

0 < T < TB

Sd (T1)

T ( 2.5 h - 2 ) : Sd (T) = a g g1 S 32 + T R 3 B

TB < T < TC

h : Sd (T) = a g g1 S 2.5 R

TC < T < TD

: Sd (T) = a g g1 S 2.5 R

TC h > 0.20 a g g1 T

TC TD h TD < T < 4.0 Sec : Sd (T) = a g g1 S 2.5 > 0.20 ag g1 2 R T TB ,TC ,TD , S , a g 5.00

Response modification factor (R) 1.00

Damping factor (h)

Prestressed Concrete Importance factor (g1) C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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l = Correction factor If T1 < 2 TC

l = 0.85

If T1 > 2 TC

l = 1.00

W = Total weight of the structure above foundation level W = S (w i ) wi = ( i ) +

+

+

+

wi = ( D.L. + a L.L.) Floor Area + O.W. of beams and columns wi = ( g s + a Ps ) Floor Area + O.W. of beams and columns

a= a 0.25 0.50 1.00

NOTE - D.L. ( g s ) & L.L. ( Ps ) are working loads ( working loads ) ‫ﻮن‬ g s = t s gc + F.C. + walls 2 If given in kN/m P s = L.L. C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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‫ﺟﻤﯿ ﻊ اﻷﺣﻤ ﺎل ﯾﺠ ﺐ أن ﺗﻜ‬

Page No.


NOTE

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Steps of Calculating Seismic Load: +

Fb = Sd (T1) 1 Calculate

T1 = Ct H

3/4

l W g

Structural System Reinforced concrete moment resisting frames (Space frames) Ductile frames (beams & columns) Non-ductile frames (flat slabs)

H

All other buildings Cores or Shear walls Combinations of (cores or shear walls) & frames

Ct 0.075

0.050

2 Subsoil Soil Class Type

3 Sd (T1 )

A

Rock

B

Dense Soil

C

Meduim Soil

D

Loose Soil

R , h ,g1 ,TB ,TC ,TD , S , a g

For Type (1) Subsoil Class A B C D Importance Category

Soil Description

For Type (2) S 1.00 1.35 1.50 1.80

TB 0.05 0.05 0.10 0.10

TC 0.25 0.25 0.25 0.30

Type of Structures

TD 1.20 1.20 1.20 1.20 Importance Factor (g1 )

I

1.40

II

1.20

III

1.00

IV

0.80

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Subsoil Class A B C D

Zone Zone 1 Zone 2 Zone 3 Zone 4 Zone 5A Zone 5B

S 1.00 1.20 1.25 1.35

TC 0.40 0.50 0.60 0.80

Design acceleration (a g ) 0.10 g 0.125 g 0.15 g 0.20 g 0.25 g 0.30 g

1.00 5.00

)

TB 0.15 0.15 0.20 0.20

(h) (R)

Page No.

TD 2.00 2.00 2.00 2.00


T1

4

Range

Sd (T1) T ( 2.5 h - 2 ) : Sd (T) = a g g1 S 23 + T R 3 B

0 < T < TB TB < T < TC

h : Sd (T) = a g g1 S 2.5 R

TC < T < TD

: Sd (T) = a g g1 S 2.5 R

TC h > 0.20 a g g1 T

TC TD h TD < T < 4.0 Sec : Sd (T) = a g g1 S 2.5 > R T2

5 Get l = 0.85

T1 < 2 TC

l = 1.00

T1 > 2 TC

6 Calculate

0.20 ag g1

W

W = S (w i ) wi = ( i ) +

+

+

+

wi = ( D.L. + a L.L.) Floor Area + O.W. of beams and columns wi = ( g s + a Ps ) Floor Area + O.W. of beams and columns a 0.25 0.50 1.00

NOTE - D.L. ( g s ) & L.L. ( Ps ) are working loads ( working loads ) ‫ﻊ اﻷﺣﻤ ﺎل ﯾﺠ ﺐ أن ﺗﻜ ﻮن‬ C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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‫ﺟﻤﯿ‬

Page No.


Distribution of lateral force on each floor ( In Elevation)

( In Plan) sw 1 sw 2

F1-5

sw 3

Fb

F1-4

sw 4

F5 F4 F3

F2-5 F2-4

F1-3

F2-3

F1-2

F2-2

F1-1

F2

F2-1

sw1

F1

sw2

F3-5

F4-5

F3-4

+

Fi = Fb

w i Hi wi Hi

F4-4

F3-3

F4-3

F3-2

i=n

F4-2

F3-1

i=1

F4-1

sw3

where: Fi = ( i )

sw4 h8

Fb = Ultimate base shear force

+

Fb = Sd (T1) Hi =

h7 h6

l W g

H5 H4

‫ ( ﻣﻘﺎﺳ ﺎً ﻣﻦ ﻣﻨﺴ ﻮب اﻷﺳﺎﺳ ﺎت‬i ) ‫ارﺗﻔ ﺎع ﺑﻼﻃ ﺔ اﻟ ﺪور رﻗ ﻢ‬

H3 H2 H1

wi = ( i )

h5 h4 h3 h2 h1

+

+

+

+

wi = ( D.L. + a L.L.) Floor Area + O.W. of beams and columns wi = ( g s + a Ps ) Floor Area + O.W. of beams and columns D.L. ( g s ) & L.L. ( Ps ) are working loads ( working loads ) ‫ﻊ اﻷﺣﻤﺎل ﯾﺠ ﺐ أن ﺗﻜ ﻮن‬ C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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‫ﺟﻤﯿ‬

Page No.


F8 F7 F6 F5 F4 F3

Fb

F2 F1

Total seismic load

Story Forces

F8

h8

F7

h7

F6

h6

F5

h5

H5

F4

h4

H4

F3

h3

H3

F2

h2

H2

F1

H1

h1

Load Diagram Q 8 = F8 Q 7 = Q 8+ F7

+

M8 = Q 8

Q 6 = Q 7+ F6

+

M7 = M 8 + Q 7 h 7

Q 5 = Q 6+ F5

+

M6 = M 7 + Q 6 h 6

Q 4 = Q 5+ F4

+

M5 = M 6 + Q 5 h 5

Q 3 = Q 4+ F3

+

M4 = M 5 + Q 4 h 4

Q 2 = Q 3+ F2

+

M3 = M 4 + Q 3 h 3

Q 1 = Q 2+ F1

M2 = M 3 + Q 2 h 2 +

Fb = S F i

h8

+

Mbase U.L.= M 2 + Q1 h 1

Overturning Moment

Shear Diagram

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+

+

+

+

+

Mbase U.L.= M2 + Q 1 h 1 =S Fi H i = F1 H 1 + F2 H 2 + F3 H 3 + ............... )

Page No.


wi (kN)

Hi (m)

wi Hi +

Fi (kN)

w8

H8

w8 H 8 +

F8

Q8 = F8

M8 = Q 8 h 8

7

w7

H7

w7 H 7 +

F7

Q 7 = Q 8 + F7

M7 = M 8 + Q 7 h 7

6

w6

H6

w6 H 6 +

F6

Q 6 = Q 7 + F6

M6 = M 7 + Q 6 h 6

5

w5

H5

w5 H 5 +

F5

Q 5 = Q 6 + F5

M5 = M 6 + Q 5 h 5

4

w4

H4

w4 H 4 +

F4

Q 4 = Q 5 + F4

M4 = M 5 + Q 4 h 4

3

w3

H3

w3 H 3 +

F3

Q 3 = Q 4 + F3

M3 = M 4 + Q 3 h 3

2

w2

H2

w2 H 2 +

F2

Q 2 = Q 3 + F2

M2 = M 3 + Q 2 h 2

1

w1

H1

w1 H 1

F1

Q 1 = Q 2 + F1

M base U.L.= M 2 + Q 1 h 1

S wi H i

S Fi

SQ

where: Floor No. = ‫ﺬ‬

i

+

SH

M i (kN.m)

+

+

+

+

+

+

+

Q i (kN)

+

+

Floor No. 8

i

‫ﺎت و ﻟﯿ ﺲ ﻟ ﻸدوار ﻟ ﺬﻟﻚ ﻓ ﻲ ﺣﺎﻟ ﺔ وﺟﻮد ﺑ ﺪروم ﺗﺄﺧ‬

‫ﺮﻗﯿﻢ ﻟﻠﺒﻼﻃ‬

‫ھﻮ ﺗ‬

( ) ‫ﺑﻼﻃ ﺔ اﻟﺒ ﺪروم رﻗ ﻢ‬

wi = ( i ) +

+

+

+

wi = ( D.L. + a L.L.) Floor Area + O.W. of beams and columns wi = ( g s + a Ps ) Floor Area + O.W. of beams and columns h8 h7

Hi =

wi H i = +

h6

‫ ( ﻣﻘﺎﺳ ﺎً ﻣﻦ ﻣﻨﺴ ﻮب اﻷﺳﺎﺳ ﺎت‬i ) ‫ارﺗﻔ ﺎع ﺑﻼﻃ ﺔ اﻟ ﺪور رﻗ ﻢ‬ H5

w i Hi w i Hi

‫ﻹﯾﺠ ﺎد اﻟﻤﻌﺎﻣ ﻞ‬

i=n

h4

H4

‫و ﯾﺘ ﻢ ﺣﺴ ﺎﺑﮭﺎ‬w i & H i ‫ھﻮ ﺣﺎﺻ ﻞ ﺿ ﺮب اﻟﻌﻤ ﻮدﯾﻦ‬

h3

H3

h2

H2 H1

h1

i=1

w i Hi = w i Hi

i=n

‫ﺔ‬

‫ ﻋﻠ ﻰ اﻷدوار اﻟﻤﺨﺘﻠﻔ‬base shear (F ) ‫ﺒﺔ اﻟ ﺘﻰ ﯾﺘ ﻢ ﺑﮭ ﺎ ﺗﻮزﯾ ﻊ‬ b

‫و ھﻲ اﻟﻨﺴ‬

i=1

i=1

+

wi & wi H i - ‫ﻮدﯾﻦ‬ w i Hi H = i=n i i=n w i Hi Hi

‫و ذﻟ ﻚ ﻷن‬

‫ﻓ ﻲ ﺣﺎﻟ ﺔ ﺗﺴ ﺎوي وزن اﻷدوار ﻻ داﻋﻲ ﻹﺿ ﺎﻓﺔ اﻟﻌﻤ‬

i=1

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h5

Page No.


Fi = ( i ) +

Fi = Fb

wi H i i=n wi Hi i=1

+

Fb = Ultimate base shear force Fb = Sd (T1) l W g Q i = ‫ﺰﻟﺰال‬

‫ﺔ ﻟﻠ‬

‫ﺄﺛﯿﺮ اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫ﺔ ﻟﻠ ﺰﻟﺰال‬

Mi =

‫ﻗ ﻮى اﻟﻘ ﺺ اﻟﻨﺎﺗﺠ ﺔ ﻣﻦ ﺗ‬

‫ﺄﺛﯿﺮ اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫اﻟﻌ ﺰوم اﻟﻨﺎﺗﺠ ﺔ ﻣﻦ ﺗ‬

‫ ﻋﻦ ﻃ ﺮﯾﻖ اﺳ ﺘﺨﺪام اﻟﻘ ﺎﻧﻮن اﻵﺗ ﻲ‬Q ‫ﺎب‬ i ‫ ﺑ ﺪون ﺣﺴ‬M

- ‫ﺎب‬ i ‫ﯾﻤﻜ ﻦ ﺣﺴ‬

+

+

+

+

Mbase U.L.=S Fi H i = F1 H 1 + F2 H 2 + F3 H 3 + ....................

Check Overturning F8

+

Mbase U.L. S Fi H i Moverturning = 1.40 = 1.40 +

Mstability = W

F7 F6 F5 F4 F3

B 2

Fb

F2

W

F1

where: W = Total weight of structure ‫ﺄ‬

Moverturning

B

‫اﻟ ﻮزن اﻟﻜﻠ ﻲ ﻟﻠﻤﻨﺸ‬

Factor Of Safety = Stability Moment

Overturning Moment

F.O.S.

=

Mstability < 1.5 Moverturning

‫( ﻛ ﺎﻵﺗﻲ‬M overturning ) - ‫ﺔ ﺣﺴ ﺎب‬

+

Mbase U.L. = ( Fb )

2H 3

‫و ذﻟ ﻚ ﺑﺸ ﺮط أن ﯾﻜ ﻮن وزن ﺟﻤﯿ ﻊ‬

Moverturning = 2H 3

‫ﺎً ﻋﻨ ﺪ‬

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‫ﺔ ﺗﺆﺛ ﺮ ﺗﻘﺮﯾﺒ‬

‫ﺔ ﺗﻘﺮﯾﺒﯿ‬

‫ﯾﻤﻜ ﻦ ﺑﻄﺮﯾﻘ‬

Mbase U.L. 1.40 ‫ﺎر أن اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫و ذﻟ ﻚ ﺑﺎﻋﺘﺒ‬

‫ﻣﺘﺴ ﺎوي‬. (wi) ‫اﻷدوار‬

)

Page No.


Check Sliding Fb 1.40 Resisting Force = m W where: W = Total weight of structure Sliding Force =

+

Fb

‫ﺄ‬

‫اﻟ ﻮزن اﻟﻜﻠ ﻲ ﻟﻠﻤﻨﺸ‬

m W +

m

W

= Coefficient of friction Factor Of Safety =

Resisting Force

< 1.5

Sliding Force

NOTE Ultimate loads Working loads

1.40

Mbase U.L. & Fb

Check sliding and Check overturning

Moverturning = Fsliding

Mbase U.L. 1.40

Fb = 1.40

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)

Page No.


Example. A ten floor hospital located in Cairo with dimensions (20 x 40 m). Height of each floor is 4.0 m. Soil below the building is very dense sand and its coeff. of friction is 0.3. All floors are flat slab of average thickness equal 0.3 m. Due to Earthquake loads , it is required to :

1- Calculate the ultimate base shear force . 2- Calculate the story shear and overturning moment at each floor level and draw its distribution on the height of the building. 3- Find the bending moment and shearing forces acting at base level of the building and draw distribution of shear forces. 4- Check The Stability of the building against silding and overturning. Given that : 4 +10 = 40 m

F.C. = 2.0 kN/m 2 Walls = 3.0 kN/m 2 L.L. = 3.0 kN/m 2

Elevation 40 m

20 m

0.30

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)

Page No.


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Cairo

Map Page (8)

Zone (3)

Very dense sand

Table Page (9)

Table Page (7)

a g = 0.15 g

Soil type (B)

Soil type (B) Table Page (9)

Response spectrum curve Type (1)

T1 = Ct H

S = TB = TC = TD =

3/4

Shear wall

Table Page (13)

C t = 0.05

Total Height of building (H) = 40 m +

T1 = 0.05

40

3/4

= 0.795 sec.

Check

T1 < ( 4 TC = 1.0 sec.)

O.K.

Sd (T)

T1 < 2.0 sec.

O.K.

2.5 ag S g1

Response Spectrum Curve

ag S g1 Sd (T) 1

TB TC

T1

TD

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4.0

)

Time (Sec) Page No.

1.35 0.05 0.25 1.20


TC < T1 < TD

Page (14)

TC h > 0.20 a g g1 T1

Sd (T1) = a g g1 S 2.5 R R = 5.00 h = 1.00 Table Page (10)

2.5 5.00

0.25 0.795

+

1.35

+

+

Sd (T1) = 0.15 g 1.40

+

g1 = 1.40 1.00

= 0.0446 g 0.20 a g g1 = 0.20

+

+

0.15 g 1.40 = 0.042 g < Sd (T1) O.K. T1 > 2 TC = 0.50 sec l = 1.00 +

ws = D.L. + a L.L. +

ws = ( t s gc + F.C. + Walls ) + a L.L. Table Page (15)

a = 0.50 +

+

+

+

+

ws = ( 0.30 25 + 2.0 + 3.0 ) + 0.50 3.0 = 14.0 kN/m2 wFloor = 14.0 20 40 = 11200 kN wTotal = 11200 10 = 112000 kN NOTE t av

t av

l W g

+

= 0.0446 g

1.0 112000 g

+

+

Fb = Sd (T1 )

Fb = 4995.2 kN C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


2- Distribution of lateral force on each floor +

Fi = Fb

w i Hi w i Hi i=1

i=n

w i Hi H = i=n i w i Hi i = 1 Hi i=1

i=n

‫ﻷن وزن اﻟ ﺪور ﺛﺎﺑ ﺖ‬

i = 10

H = 40 + 36 + 32+ 28 +24+ 20 +16 + 12 + 8 + 4 i i=1 = 220 m Fi = ( 4995.2 ) 1 H i 220

36 28 20

Fi

=

16

22.705 H i

12 4

Floor H (m) F (kN) Q (kN) i i i No. 40.0 908.22 908.22 10

8

Mi (kN.m) 3632.87

9

36.0

817.40 1725.62

10535.33

8

32.0

726.57 2452.19

20344.09

7

28.0

635.75 3087.94

32695.85

6

24.0

544.93 3632.87

47227.35

5

20.0

454.11 4086.98

63575.27

4

16.0

363.29 4450.27

81376.35

3

12.0

272.47 4722.74 100267.29

2

8.0

181.64 4904.38 119884.80

1

4.0

90.82

4995.20 139865.60

Shearing force at base = 4995.2 kN C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.

24

32

40


908.22

908.22

1725.62

817.40

3632.87

2452.19

726.57

10535.33

3087.94

635.75

20344.09

3632.87

544.93

32695.85

4086.98

454.11

47227.35

4450.27

363.29

63575.27

4722.74

272.47

81376.35

4904.38

181.64

100267.29

4995.20

90.82

119884.80 139865.60

Shear Diagram

Load Diagram

Moment Diagram

3- Check sliding Fb = 4995.2 = 3568 kN 1.40 1.40

Factor Of Safety =

W = 0.30 112000 = 33600 +

Resisting Force =m

+

Sliding Force =

Resisting Force Sliding Force =

33600 3568

= 9.4 > 1.5 Safe

4- Check overturning Mbase U.L. = 139865.6 kN.m 1.40

= 139865.6 = 99904 kN.m 1.40 +

Resisting Moment = WTotal

B 112000 2 =

+

Moverturning =

Mbase U.L.

Resisting Moment

Factor Of Safety = Over Turning Moment =

20 1120000 kN.m 2 = 1120000 11.2 > 1.5 99904 =

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)

Page No.


2. Wind Loads. ‫ھﻲ اﻟﻘ ﻮى اﻟ ﺘﻲ ﺗﺆﺛ ﺮ ﺑﮭ ﺎ اﻟﺮﯾ ﺎح ﻓ ﻲ اﺗﺠ ﺎه ﻣﺘﻌﺎﻣ ﺪ ﻋﻠ ﻰ أﺳ ﻄﺢ اﻟﻤﻨﺸ ﺄت‬ Ce = - 0.8 Pressure

(0.00)

Elevation

Wind load acting on the structure

kN/m

‫ﺿ ﻐﻂ اﻟﺮﯾ ﺎح اﻟﻤﺆﺛ ﺮ ﻋﻤﻮدﯾ ﺎً ﻋﻠ ﻰ وﺣﺪة‬ ‫ﺄ‬

Ce = - 0.5

Ce = - 0.7

2

C e = + 0.8

where: Pe =

+

+

Pe = C e k q

Ce = - 0.5

(0.00)

Ce = + 0.8

Suction

‫اﻟﻤﺴ ﺎﺣﺎت ﻋﻠ ﻰ اﻷﺳ ﻄﺢ اﻟﺨﺎرﺟﯿ ﺔ ﻟﻠﻤﻨﺸ‬ Ce = - 0.7

Ce =

‫( أو ﺳ ﺤﺐ‬Pressure) ‫ﻣﻌﺎﻣﻞ ﺗﻮزﯾ ﻊ ﺿ ﻐﻂ‬

Plan

‫( اﻟﺮﯾ ﺎح ﻋﻠ ﻰ اﻷﺳ ﻄﺢ اﻟﺨﺎرﺟﯿ ﺔ‬Suction)

C e = 0.8 + 0.5 = 1.3

k = Factor of exposure

Ground Roughness Length Zone (A): Zone (B):

Open exposure Suburban exposure

Zone (C): City center exposure C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


Zone Ground roughness length Height (m) 0 - 10 10 - 20 20 - 30 30 - 50 50 - 80 80 - 120 120 - 160 160 - 240

A

B

C

0.05

0.30

1.00

1.00 1.15 1.40 1.60 1.85 2.10 2.30 2.50

k 1.00 1.00 1.00 1.05 1.30 1.50 1.70 1.85

1.00 1.00 1.00 1.00 1.00 1.15 1.30 1.55

(Most critical case)

NOTE

(Open exposure or Suburban exposure or City center exposure) (Ground roughness length = 0.05 or 0.30 or 1.00) (Zone A) k (Most critical case)

q (kN/m ) 2

q

2 0.5 r V C t Cs = 1000

2

kN/m

where: V (m/sec)

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)

Page No.


V (m/sec) 42 39 36 33 30

r=

1.25 kg/m 3 C t = Factor of topography Ct 1.00 1.20 1.40 1.60 1.80 1.80 1.00

:

1.80 NOTE 1.00

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Ct

)

Page No.


C s = Structural factor Turbulence

:

1.00

1.00

Cs

NOTE C s & Ct V 2

+

+

+

q = 0.5 r V C t Cs = 0.5 1.25 1.00 1.00 V 2 1000 1000 +

q = 6.25 10-4 V 2

q

(kN/m) 2

1.10 0.95 0.81 0.68 0.56 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


kN kN

+ +

+ +

Wind load (F) = Pe area = C e k q area where: area = Area subjected to wind

‫اﻟﻤﺴ ﺎﺣﺔ اﻟﻤﻌﺮﺿ ﺔ ﻟﻠﺮﯾ ﺎح‬

NOTE ‫ﺄﺛﯿﺮ ﺣﻤﻞ اﻟ ﺰﻟﺰال و اﻟﻌﻜ ﺲ و ذﻟ ﻚ ﻷن ﺣ ﺪوﺛﮭﻤﺎ‬

‫ﺎ ﻻ ﻧﺄﺧ ﺬ ﺗ‬

‫ﺄﺛﯿﺮ ﺣﻤﻞ اﻟﺮﯾ ﺎح ﻓﺈﻧﻨ‬

‫ﻋﻨ ﺪﻣﺎ ﻧﺄﺧ ﺬ ﺗ‬ ً‫ﻣﻌ ﺎً ﻧ ﺎدر ﺟ ﺪا‬.

Distribution of wind +

+

Pe = C e k

q

2

kN/m ( P ) kN\m (Most critical case) 4 Zone A ( P ) kN\m 3 k 4 = 1.60 q ( P2 ) kN\m k 3= 1.40 q k 2= 1.15 q ( P1 ) kN\m q k 1 = 1.00 2

2

+

+

k4 k3 k2 k1

+ +

+ +

+

+

P4 = Ce P3 = Ce P2 = Ce P1 = Ce

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2

2

)

h4 h3

H h2 h1

Page No.


+ + +

F4

kN

+

(h4 b ) (h3 b ) +

F3 kN

(h2 b ) (h1 b )

H4

F2 kN

+

+

+

+

F4 = P4 F3 = P3 F2 = P2 F1 = P1

H3

+

+

b

q area

F= Ce k

F1

H2

kN

h

4

h

3

h

2

h

H1

H

1

+

+

+

+

Total Moment at base = S Fi H i M overturning = F1 H 1 + F2 H 2 + F3 H 3 + .................... NOTE Working loads Check sliding and Check overturning

Difference between wind & seismic loads: Wind loads

Seismic loads

‫ﺔ ﻓ ﻲ اﺗﺠ ﺎه واﺣﺪ‬

‫ ﻗ ﻮة أﻓﻘﯿ‬-

‫ ﻗ ﻮة ﺗﮭ ﺰ اﻟﻤﻨﺸ ﺄ ﻓ ﻲ ﺟﻤﯿ ﻊ اﻻﺗﺠﺎھ ﺎت‬-

‫ ﺿ ﻐﻂ اﻟﺮﯾ ﺎح ﯾﻌﺘﻤ ﺪ ﻋﻠ ﻰ اﻟﺴ ﻄﺢ‬‫ﺄ‬

‫ ﻗ ﻮة اﻟ ﺰﻟﺰال ﻧﺴ ﺒﺔ ﻣﻦ وزن اﻟﻤﻨﺸ ﺄ‬-

‫اﻟﺨ ﺎرﺟﻲ ﻟﻠﻤﻨﺸ‬

‫ ﻗ ﻮة اﻟﺮﯾ ﺎح ﺗﺆﺛ ﺮ ﻋﻠ ﻰ اﻟﻮاﺟﮭﺔ ﺣ ﺘﻰ‬-

‫ ﻗ ﻮة اﻟ ﺰﻟﺰال ﺗﺆﺛ ﺮ ﻓ ﻲ ﻣﺴ ﺘﻮى اﻟﺒﻼﻃ ﺎت ﺣ ﺘﻰ‬-

‫ﻣﻨﺴ ﻮب ﺳ ﻄﺢ اﻷرض‬

Working loads ‫ﻮن‬

‫ أﺣﻤﺎل اﻟﺮﯾ ﺎح ﺗﻜ‬-

‫ﯿﺲ‬

Ultimate loads ‫ﻮن‬

‫ﻣﻨﺴ ﻮب اﻟﺘﺄﺳ‬

‫ أﺣﻤﺎل اﻟ ﺰﻻزل ﺗﻜ‬-

(0.00)

Wind load distribution C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

Storey forces due to seismic load

)

Page No.


Factored loads of Ultimate Limit Design Method: Ultimate Load (U) : 0.8 [1.4 D.L. + 1.6 L.L. + 1.6 W.L.] U= 1.12 D.L. + a L.L. + S.L. 1.4 D.L. + 1.6 L.L.

(U)

where: D.L. = Dead load L.L. = Live load S.L. = Seismic load W.L. = Wind load

a= a 0.25 0.50 1.00

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)

Page No.


Example.

3.0 +16 = 48 m

The shown figure of a store house which lies at Cairo. The building consist of a ground , mezzanine and 16 repeated floors and two basements. It is required to : 1- Calculate the wind load acting on the building . 2- Check The Stability of the building against sliding and overturning. Given that :

3.5 3.5 4.0 4.0

t s average= 0.20 m F.C. = 2.0 kN/m 2 Walls = 3.0 kN/m 2 L.L. = 3.0 kN/m 2

Sec . Elevation 6.0 6.0 6.0 6.0 6.0 6.0

6.0

6.0

6.0

6.0

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)

Page No.


Solution Ce = 0.8 + 0.5 = 1.3 2

+ + +

+ +

+ + +

2

1.0 0.68 = 0.884 kN/m 1.15 0.68 = 1.017 kN/m2 1.40 0.68 = 1.238 kN/m2 1.60 0.68 = 1.414 kN/m2 1.85 0.68 = 1.635 kN/m 2 294.3 kN

1.635 2 kN/m

6m

+ +

+

F5 = P5 ( h b) = 1.635 6 30 = 294.3 kN +

+

+

+ + + +

q = 1.3 q = 1.3 q = 1.3 q = 1.3 q = 1.3

+ +

+

+

+

+

+

P1 = Ce P2 = Ce P3 = Ce P4 = Ce P5 = Ce

k1 k2 k3 k4 k5

+

+

+

-4 0.5 r V C t Cs 2 2 q= = 6.25 10 33 = 0.68 kN/m 1000 Zone A ( More Critical ) Pe = Ce k q (kN/m2 )

+

371.4 kN

1.2382 kN/m

10 m

1.017 kN/m2

10 m

56 m

20 m

+

+

+

F2 = P2 ( h b) = 1.017 10 30 = 305.1 kN

+

+

+

F1 = P1 ( h b) =0.884 10 30 = 265.2 kN

305.1 kN

265.2 kN

0.884 kN/m2 10 m

Total wind force = 265.2 + 305.1 + 371.4 + 848.4 + 294.3 = 2084.4 kN C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.

7m

+

1.414 kN/m2

+

+

+

F3 = P3 ( h b) =1.238 10 30 = 371.4 kN

+

848.4 kN

+

+

+

+

F4 = P4 ( h b) = 1.414 20 30 = 848.4 kN


1.635 2 kN/m

848.4 kN

371.4 kN 60

47

305.1 kN

6m

1.414 kN/m2

20 m

1.2382 kN/m

10 m

1.017 kN/m2

10 m

56 m

294.3 kN

32

265.2 kN

0.884 kN/m2

22

10 m

7m

12

Check overturning

+

+ +

+

+

+

+

+

+

+

+

Total Moment at base ( Overturning Moment ) = Fi H i = F1 H1 + F2 H2 + F3 H3 + F4 H4 + F5 H5 = 265.2 12 + 305.1 22 + 371.4 32 + 848.4 47 + 294.3 60 = 79312.2 kN.m

+

Resisting Moment = WTotal

B 2

+

+

+

+

ws = t av gc + F.C. + Walls + L.L. ws = 0.20 25 + 2.0 + 3.0 + 3.0 = 13.0 kN/m2 wFloor = 13.0 30 30 = 11700 kN wTotal = 11700 20 = 234000 kN +

Resisting Moment = 234000

30 3510000 kN.m 2 =

Resisting Moment

3510000

Factor Of Safety = Over Turning Moment = 79312.2 = 44.2 > 1.5

Safe

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)

Page No.


Check sliding

W = 0.30 234000 = 70200 +

Resisting Force =m

+

Sliding Force = wind force = 2084.4 kN

Resisting Force 70200 Factor Of Safety = Sliding Force = 2084.4

= 33.7 > 1.5 Safe

NOTE Working loads Check sliding and Check overturning

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)

Page No.


Systems resisting lateral loads. ‫ﺔ و ﻣﻨﮭﺎ‬

‫ﺎﺋﯿﺔ ﺗﻘ ﺎوم اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫ﺗﻮﺟ ﺪ ﻋﺪة أﻧﻈﻤ ﺔ إﻧﺸ‬

1- Shear walls or cores

Shear walls

Core (Tube)

2- Coupled shear walls

3- Frames

Ductile frames (Beams + Columns)

4- Combination between different systems - Frames + Shear walls - Frames + Core - Core + Shear walls - Frames + Shear walls + Cores C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

Core

Shear wall

)

Frames

Page No.


Center of Mass (C.M.) & Center of Rigidity (C.R.) ( Columns - Core - Shear Walls ) ( Slabs - Beams ) - ‫ﺔ ﻻﺑ ﺪ ﻣﻦ ﻣﻌﺮﻓ ﺔ ﺑﻌ ﺾ اﻟﻤﻔ ﺎھﯿﻢ‬

‫ﺎﺋﯿﺔ اﻟ ﺘﻲ ﺗﻘ ﺎوم اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫ﻗﺒ ﻞ دراﺳ ﺔ اﻷﻧﻈﻤ ﺔ اﻹﻧﺸ‬ ‫ﯿﺔ‬

Center of mass (C.M.):

‫اﻷﺳﺎﺳ‬

It is the center of gravity of area and it is the point of application of ( Fb ). wi Ai x i wi A i +

Datum

+

+

X C.M.= where:

+

+ +

+ +

w2 A2

C.G. C.M.

Center of rigidity (C.R.): It is the point where the force ( Fb ) is resisted. ( Stiffness ) ( Columns - Core - Shear Walls ) NOTE

(C.M.)

( C.R.)

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)

Page No.

+

w1 A1

X C.M.

w A x + w2 A 2 x 2 X C.M.= 1 1 1 w1 A1 + w2 A2 +

x1 +

XC.M.= Distance between C.M. & datum x i = Distance between C.G. of A i & datum wi = Weight of floor at this part of floor A i

x2

C.G.


(C.R. ) (Shear wall )

(C.M.) (Core) ( C.M.)

(C.R. ) (Torsion )

( C.R. )

Fb

Fb (Torsion)

C.R.

C.M.

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C.R.

)

C.M.

Page No.


1- Shear walls or cores Case (a): Symmetrical shear walls (C.M. = C.R.) Lateral Force (F b ) Ii +

Fi =

i=n i=1

Ii

C.M.

‫ ﻋﻠ ﻰ اﻟﺤ ﻮاﺋﻂ ﺑﻨﺴ‬Bending Moment ‫ أو‬Shear force

Fb & M i =

Ii

i=n

i=1

+

( Inertia ) ‫ﺒﺔ‬

C.R.

Ii

M base sw1 I1

I1 F1 = F 2I1 + 2I 2 b I2 F2 = Fb 2I1 + 2I 2 where:

sw2

sw2 I2

I2

C.M.

sw1 I1

+

C.R.

x2

x1

+

x1

x2

Fb

F b = Force acting at the base Fi = Force acting on the shear wall no. ( i ) I i = Moment of inertia of the shear wall no. ( i ) M base= Bending Moment acting at the base M i = Bending Moment acting on the shear wall no. ( i ) Case (b): Unsymmetrical shear walls in one direction (C.M. = C.R.) C.R. C.M. L To Get C.R. Datum

1

X

C.R.

Ii xi Ii

=

sw2 sw1

+

+

+

+

I1

x1

I3

e xC.M.

x2

x3

e = Distance between C.M. & C.R. C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

sw4

C.M.

I2

xC.R.

e = X C.M. X C.R.

where:

sw3

C.R.

I1 x 1+ I 2 x 2 + I 3 x 3 + I 4 x 4 X C.R.= I1 + I2 + I 3 + I 4

2

MT

Fb x4 Page No.

I4


M T = Fb e*

e *= e + 0.05 L

+

3

‫ ( ﻋﻠ ﻰ اﻟﺤ ﻮاﺋﻂ ﻛ ﺎﻵﺗﻲ‬F ) ‫ﺛ ﻢ ﺗ ﻮزع اﻟﻘ ﻮة‬ b

Ii xi MT i=n 2 I (xi ) i=1 i

+

+

Fi = i = In i Fb + Ii i=1 where:

Fb

x = (C.R.) ‫ھﻮ ﺑﻌ ﺪ اﻟﺤ ﺎﺋﻂ ﻋﻦ‬ i

sw3 C.M.

x1

I3

e

x3

x2

+

Ii Ii i=1

i=n

x4

Fb

+

Ii xi 2 I ( x ) i i i=1 i=n

I4

MT

I1 I1 x 1 Fb 2 2 2 2 I1 + I2 + I3 + I4 I 1( x1) + I2 (x2) + I 3 (x3) + I 4 (x4)

F2 =

I2 I2 x 2 Fb 2 2 2 2 I1 + I2 + I3 + I4 I 1( x1) + I2 (x2) + I 3 (x3) + I 4 (x4)

F3 =

I3 I3 x 3 Fb + 2 2 2 2 I1 + I2 + I3 + I4 I 1( x1) + I2 (x2) + I 3 (x3) + I 4 (x4)

F4 =

I4 I4 x 4 Fb + 2 2 2 2 I1 + I2 + I3 + I4 I 1( x1) + I2 (x2) + I 3 (x3) + I 4 (x4) +

+

+

+

F1 =

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)

Page No.

+

I2

MT

+

C.R.

I1

sw4

MT

+

sw1

MT

MT

+

sw2

MT


Fb

NOTE sw2 sw1

MT

sw4

sw3 C.M.

C.R.

(- ve) Zone ( 2 )

(+ ve) Zone ( 1 )

C.M. ‫ و اﻟ ﺘﻰ ﺑﮭ ﺎ‬Zone ( 1 ) ‫ إذا ﻛ ﺎن اﻟﺤ ﺎﺋﻂ ﯾﻘ ﻊ ﻓ ﻲ‬+ ve - ‫ﺣﯿ ﺚ أن اﻹﺷ ﺎرة ﺗﻜ ﻮن‬ .Zone ( 2 ) ‫ إذا ﻛ ﺎن اﻟﺤ ﺎﺋﻂ ﯾﻘ ﻊ ﻓ ﻲ‬- ve ‫و ﺗﻜ ﻮن اﻹﺷ ﺎرة‬ .C.R.

‫ ﯾﻜ ﻮن اﻟﺨ ﻂ اﻟﻤ ﺎر ﺑـ‬Zone ( 1 ) & Zone ( 2 ) - ‫ﻞ ﺑﯿ ﻦ‬

‫اﻟﺨ ﻂ اﻟﻔﺎﺻ‬

(Shear wall) ‫ ( ﯾﻤﻜ ﻦ إﯾﺠ ﺎد ﻧﺴ ﺒﺔ اﻟﻘ ﻮى اﻟﻤﺆﺛ ﺮة ﻋﻠ ﻰ ﻛ ﻞ‬F = 1 kN ) - ‫ﺎﻟﺘﻌﻮﯾﺾ ﻋﻦ‬ b

+

M i = % of each Shear Wall

+

Ii xi (1 2 I (x i) i=1 i

i=n

+

+

% of each Shear Wall = i = In i 1 + Ii i=1

‫ﺑ‬

e* )

M base

Case (c): Unsymmetrical shear walls in both direction (ey ) & (ex )

( Eccentricity ) ( C.R.)

( I y ) & ( Ix )

(I)

y

Lx sw3

Fby e *x +

sw1

xC.M.

sw4

xC.R.

Fbx

Ly

C.M.

Fbx

+

x1

e *y

ey C.R.

ex

sw2

y2

x4

y3 yC.R. yC.M.

x

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)

Page No.


e x* = e + 0.05 L x

1 2

(sw3 ) & (sw2) Y = Iy i yi = I y2 y2 + Iy3 y3 C.R. Iy i Iy2 + Iy3 e y = Y C.M. - Y C.R.

3

e y* = e + 0.05 L y

( Fby )

+

3

+

M T y = Fby e*x ( Fbx)

+

+

M T x = Fbx e*y +

1

+

2

(sw4 ) & (sw1) X = Ix i xi = Ix1 x 1 + Ix 4 x 4 C.R. Ix i Ix1+ Ix4 e x = X C.M. - X C.R.

y

Lx sw3

sw1

x1

Fbx

ey sw 2

i=n i=1 i=n

x4 C.M.

sw4

y

Ly

3

C.R.

ex

y2

2

2

2

2

2

2

x

Ix i (x i) = I x1 (x1) + Ix 4 (x4)

Fby

Iy i (y i) = I y2 (y2 ) + Ix 3 (y3 ) i=1

M Ty

Iy i yi 2 2 [ I ( x ) + I ( y ) y x i i i i i=1

M Tx

i=n

+

( C.M. ) ( C.M. )

+

Fx = i = In yi Fbx + i Iy i i=1

+

i=n

+

Ix i xi 2 2 [ I ( x ) + I ( y ) x y i i i i i=1

Fy = i = In xi Fby + i Ix i i=1

( Shear wall ) ( Shear wall )

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(+ ) ( )

)

Page No.


NOTE

sw1

Symmetric

e *= 0.05 L

M T = Fb e* sw2

sw2

I1

I2

I2

D.L.

T.L.

T.L. sw1

+

e min = 0.05 L

sw1

I1

I1

sw1

sw1

I1

I1

I2 C.R.

e min

I2

x1

I2

sw1 I1

emin

C.M.

= 0.05L

x2

x1

x1

x2

x2

x1

Fb

Ii xi i=n 2 I ( x ) i i=1 i

+

+

sw2 C.R.

Fb

Fi = i = In i Fb + Ii i=1

I1

C.M.

I2

OR

C.M.

sw1

D.L.

sw2

= 0.05L

x2

I2

T.L. sw2

I2

sw2

sw2

T.L.

C.M.

sw2

I1

sw1

MT

‫ ( ﻋﻠ ﻰ اﻟﺤ ﻮاﺋﻂ ﻛ ﺎﻵﺗﻲ‬F ) ‫ﺛ ﻢ ﺗ ﻮزع اﻟﻘ ﻮة‬ b

where: x = (C.R.) ‫ھﻮ ﺑﻌ ﺪ اﻟﺤ ﺎﺋﻂ ﻋﻦ‬ i

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)

( 0.05 L Fb )

+

Fb +

( 0.05 L Fb ) +

I2 2 ( I1 + I2 )

+

F2 =

Fb +

More Critical I1 x 1 2 2 2 [ I 1( x1) + I 2 (x2) ] I2 x 2 2 2 2 [ I 1( x1) + I 2 (x2) ]

+

I1 2 ( I1 + I2 )

+

F1 =

+

e min

Page No.


Illustrative Example For the shown figure , if the thickness of all shear walls = 25 cm . It is required to : 1- Calculate the percentage of force ( P ) acting on each wall

Solution 3

3.5

2.5

sw1

sw2

+

Isw1 = 0.25 (3.5) = 0.8932 m4 12

sw3

4.0

3

+

I sw2 = 0.25 (2.5) = 0.3255 m4 12

Fb

15

3

+

I sw 3 = 4.0 ( 0.25 ) = 0.0052 m4 12

sw3

i=6

i=6 i=1

I

I sw 2 i=6 i=1

I

Isw 3 i=6 i=1

I

sw2

sw1

I = 2 ( 0.8932 + 0.3255 + 0.0052 ) i=1 4 = 2.4478 m

Isw 1

4.0

3.5

10.0 m

0.8932 = 2.4478 = 36.50 % 0.3255 = 2.4478 = 13.3 % 0.0052 = 0.20 % = 2.4478

( Inertia )

( sw3 )

NOTE Shear wall Fb

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)

Page No.

2.5


Design of Shear wall. Shear walls solved as a cantilever totally fixed in foundation and subjected to moment (M ) due to lateral force and normal force ( N ) due to own weight ,weight of walls and floors . 2 sw

F6 F5 F4

1 sw

sw 3

sw 6

sw 4

F6 F5

sw 5

F3 F2 F1

F4 F3

Elevation

F2 F1

sw1

sw2 sw3

Fi F 6-2

sw4

F 5-2

sw6

sw5

F 4-2

Plan

F 2-2

Fsw =

F 1-2

i

i=n i=1

Shear Wall 2 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

I sw i

)

+

F 3-2

Fi

I sw i

Page No.


= % of each Shear Wall

+

+

MS.L.= % of each Shear Wall M

Base Seismic U.L.

N

load

+

+

M W.L.= % of each Shear Wall M Base Wind Working = % of each Shear Wall

Fi H i Fi H i

= O.W of shear wall + The Normal Force Due to Seismic or Wind Loads

+

+ The part from the floor which it carry

number of floors

Cases of Load Combinations Case (1) D.L.+L.L.

Case (2) D.L.+L.L.+W.L.

Case (3) D.L.+L.L.+S.L.

N = 1.4 N D.L.+ 1.6 N L.L. M = 1.4 M D.L.+ 1.6 M L.L. N = 0.8 [1.4 ND.L.+ 1.6 N L.L.+ 1.6 NW.L.] M = 0.8 [1.4 MD.L.+ 1.6 M L.L.+ 1.6 M W.L.] N = 1.12 ND.L.+ a N L.L.+ N S.L. M = 1.12 M D.L.+ a M L.L.+ M S.L.

where: a=

a 0.25 0.50 1.00

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)

Page No.


NOTE

Working

Manual

MW.L.

Ultimate

MS.L.

Seismic & Wind SAP

N W.L.= Zero

and

N S.L.= Zero D.L. & L.L. Flat Slabs

Moments Frames

Cases of Load Combinations Case (1) N = 1.4 N D.L.+ 1.6 N L.L. Case (2) N = 0.8 [1.4 ND.L. + 1.6 N L.L.] & M = 0.8 [1.6 M W.L.] Case (3) N = 1.12 ND.L.+ a N L.L.

Design of Shear wall under M & N

e t

<

1

0.5

+

Msu = N u.l.

0.225

J

Get

0.15 b d 100

st. 360/520

N u.l. = Fcu b t Fcu b t 2

As= As = ( \

Get

= -4

cu

F 0.6 As = Ac min 100

As min= 1.3A s req st. 240/350

e < 0.5 t

M u.l.

Fcu b d > 1.1 b d Fy Fy

0.25 b d 100

Mu.l. N u.l.

Using interaction diagram As = As\ take x = 0.9

+ +

+

e= 2

e s = e + 2t - c es

Mus C1 Fcu b M us Nu.l. As = J d Fy ( Fy / s ) d = C1

M = M S.L.

&

As

10 ) b t

As

b t C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


2- Rigid frames frames ‫ﺾ ﻟﻜ ﻲ ﺗﻜ ﻮن‬

‫ھﻲ ﻋﺒ ﺎرة ﻋﻦ ﻣﺠﻤﻮﻋﺔ ﻣﻦ اﻟﻜﻤ ﺮات و اﻷﻋﻤ ﺪة ﻣﺘﺼ ﻠﺔ ﺑﺒﻌ‬ ‫ ﻟﻤﻘﺎوﻣ ﺔ اﻟﻘ ﻮى اﻷﻓﻘﯿ‬frames ‫ﺘﺨﺪم ھﺬه‬

‫ﺔ و ﻓ ﻲ ھﺬه اﻟﺤﺎﻟ ﺔ ﯾﺠ ﺐ أن ﺗﺼ ﻤﻢ اﻟﻮﺻ ﻠﺔ‬ ‫ﺔ‬

‫ﺘﻄﯿﻊ ﻣﻘﺎوﻣﺔ اﻷﺣﻤ ﺎل اﻷﻓﻘﯿ‬

‫و ﺗﺴ‬

‫ﻟﻜ ﻲ ﺗﺴ‬. (rigid frames) ‫ﺑﯿ ﻦ اﻟﻌﻤ ﻮد و اﻟﻜﻤ ﺮة ﻋﻠ ﻰ أﻧﮭ ﺎ‬

point of zero moment

B.M.D due to Hz. loads

Rigid Frames

Rigid Frames

Fb

Plan C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


‫‪NOTE‬‬ ‫ﯾﺠ ﺐ أن ﺗﻜ ﻮن أﻃﻮال ﺟﻤﯿ ﻊ وﺻ ﻼت اﻟﺤﺪﯾ ﺪ )‬ ‫‪.‬ﺗﺤﻤ ﻞ اﻟﻌ ﺰوم اﻟﻨﺎﺗﺠ ﺔ ﻋﻦ اﻟﻘ ﻮى اﻷﻓﻘﯿ‬

‫‪ (L d= 60‬أي وﺻ ﻼت ﺷ ﺪ ﻟﻜ ﻲ ﺗﺴ‬

‫ﺘﻄﯿﻊ‬

‫ﺔ‬

‫ﯾﺠ ﺐ ﻋﻤﻞ ﺟﻤﯿ ﻊ وﺻ ﻼت اﻟﺤﺪﯾ ﺪ ﻟﻸﻋﻤ ﺪة ﻋﻨ ﺪ ﻣﻨﺘﺼ ﻒ اﻟ ﺪور )‪(point of zero moment‬‬ ‫ﻧﻈ ﺎم )‪ (rigid frames‬ﯾﺼ ﻠﺢ ﻟﻤﻘﺎوﻣ ﺔ اﻷﺣﻤ ﺎل ﺣ ﺘﻰ‬ ‫اﻷﻓﻘﯿ‬

‫ﺔ ﻛﺒ‬

‫ﯿﺮة ﻧﺴ‬

‫دور و ﻟﻜ ﻦ ﺗﻜ ﻮن اﻹزاﺣﺔ‬

‫ﺒﯿﺎً ﻟ ﺬﻟﻚ ﯾﺠ ﺐ ﺣﺴ ﺎﺑﮭﺎ‬

‫وﺻ ﻼت اﻟﺤﺪﯾ ﺪ ﻟﻸﻋﻤ ﺪة‬ ‫ﻋﻨ ﺪ ﻣﻨﺘﺼ ﻒ اﻻرﺗﻔ ﺎع‬

‫‪Ld = 60‬‬

‫‪Ld = 60‬‬

‫‪Ld = 60‬‬ ‫‪Ld = 60‬‬

‫‪Details of RFT of a rigid joint‬‬ ‫ﻋﻨ ﺪ اﺳ ﺘﺨﺪام ‪Core & Shear walls‬ﻛﺎﻧ ﺖ اﻟﻘ ﻮة اﻷﻓﻘﯿ‬

‫ﺔ ) ‪Base shear ( Fb‬‬

‫و اﻟﻌ ﺰوم اﻟﻨﺎﺗﺠ ﺔ ﻋﻨﮭ ﺎ‪ M base‬ﺗ ﻮزع ﻋﻠ ﻰ اﻟﻌﻨﺎﺻ ﺮ اﻟﻤﻘﺎوﻣ ﺔ ﺑﺪﻻﻟ ﺔ ) ‪Inertia ( I‬‬ ‫ﺑﯿﻨﻤ‬

‫ﺎ ﻋﻨ ﺪ اﺳ ﺘﺨﺪام ‪ Rigid frames‬ﺗ ﻮزع اﻟﻘ ﻮة اﻷﻓﻘﯿ‬

‫ﺔ )‪Base shear ( Fb‬‬

‫و اﻟﻌ ﺰوم اﻟﻨﺎﺗﺠ ﺔ ﻋﻨﮭ ﺎ‪ M base‬ﻋﻠ ﻰ اﻟﻌﻨﺎﺻ ﺮ اﻟﻤﻘﺎوﻣ ﺔ ﺑﺪﻻﻟ ﺔ ) ‪Stiffness ( K‬‬

‫‪Page No.‬‬

‫)‬

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Case (a): Symmetrical rigid frames (C.M. = C.R.) Lateral Force (Fb ) (stiffness of each frame) ‫ﺒﺔ‬

C.R.

C.M.

‫( ﺑﻨﺴ‬Frames) ‫ ﻋﻠ ﻰ‬Bending momen ‫ أو‬Shear force

To get stiffness of each frame:

Fb

For typical story 1 2I c1 1+ h ( Ibb1 + Ibb2 ) 1 2

12EI K int.= 3 c1 h

K ext.=

1 2I c2 h ( Ibb1 ) 1

12EI c2 1+ h3

F1

F2

h =

F1

K2

K1

C.M. C.R.

K1

K2

h Ic2

Ic1

Ib1

h Ic2

where:

F2

Ib2

Ic2

Ic1 b1

‫ارﺗﻔ ﺎع اﻟ ﺪور‬

b2

E = 4400 Fcu K = SK Fi

+int. SK

K ext.

ext.

K int.

K ext.

KF1= 2Kext.+ Kint. ( stiffness for frame F1 ) KF2= 2Kext.+ 2K int. ( stiffness for frame F2 )

K Fi i=n i=1

K Fi

Fb

&

‫( ﺑﻨﺴ‬Frames) ‫ ( ﻋﻠ ﻰ‬F ) ‫ﺛ ﻢ ﺗ ﻮزع اﻟﻘ ﻮة‬ b

Fi M i = i =K n i=1

+

Fi =

+

(Stiffness of each frame) ‫ﺒﺔ‬

KFi

M base

‫ﺘﻨﺘﺠﺔ ﻋﻠ ﻰ أﺳ ﺎس ﺛﺒ ﺎت ﻗﻄ ﺎع اﻟﻌﻤ ﻮد ﻓ ﻲ ﻛ ﻞ اﻷدوار‬ C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

‫ﺎﺑﻘﺔ ﻣﺴ‬

Ic2

‫اﻟﻤﻌ ﺎدﻻت اﻟﺴ‬.

Page No.


+

Case (b): Unsymmetrical rigid frames in one direction (C.M. = C.R.) C.R. C.M. L Datum To Get C.R. F1 F2 F3 F4 x 1 XC.R. = K Fi i MT K Fi C.M.

C.R.

2

+

+

+

K F1 x1 + KF2 x 2 + KF3 x 3 + K F4 x4 K F1 + KF2 + K F3 + K F4 +

X C.R.=

e = X C.M. - X C.R.

K1

K2

K3

xC.R.

e xC.M.

x1

where:

x2

x3

e = Distance between C.M. & C.R.

x4

M T = Fb e*

e * = e + 0.05 L

+

3

Fb

+

KFi xi i=n 2 K ( x ) i Fi i=1

+

Fi Fi = i = K Fb + n K Fi i=1

+

‫ ( ﻛ ﺎﻵﺗﻲ‬Frames ) ‫ ( ﻋﻠ ﻰ‬F ) ‫ﺛ ﻢ ﺗ ﻮزع اﻟﻘ ﻮة‬ b

MT

where: x = (C.R.) ‫( ﻋﻦ‬frames)

‫ھﻮ ﺑﻌ ﺪ‬

i

NOTE

F1

F2

Fb MT C.R.

(- ve) Zone ( 2 )

F3

F4

C.M.

(+ ve) Zone ( 1 )

C.M. ‫ و اﻟ ﺘﻰ ﺑﮭ ﺎ‬Zone ( 1 ) ‫ ﯾﻘ ﻊ ﻓ ﻲ‬frame ‫ إذا ﻛ ﺎن‬+ ve - ‫ﺣﯿ ﺚ أن اﻹﺷ ﺎرة ﺗﻜ ﻮن‬ .Zone ( 2 ) ‫ﯾﻘ ﻊ ﻓ ﻲ‬frame ‫ إذا ﻛ ﺎن‬- ve ‫و ﺗﻜ ﻮن اﻹﺷ ﺎرة‬

.C.R. ‫ ﯾﻜ ﻮن اﻟﺨ ﻂ اﻟﻤ ﺎر ﺑـ‬Zone ( 1 ) & Zone ( 2 ) - ‫اﻟﺨ ﻂ اﻟﻔﺎﺻ ﻞ ﺑﯿ ﻦ‬ C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.

K4


(Frame) ‫( ﯾﻤﻜ ﻦ إﯾﺠ ﺎد ﻧﺴ ﺒﺔ اﻟﻘ ﻮى اﻟﻤﺆﺛ ﺮة ﻋﻠ ﻰ ﻛ ﻞ‬F = 1kN) - ‫ﺎﻟﺘﻌﻮﯾﺾ ﻋﻦ‬

M i = % of each Frame

+

+

(1

‫ﺑ‬

e* )

M base

‫ﺎﺑﻘﺔ ﺗﻜ ﻮن ﻟ ﻼدوار اﻟﻤﺘﻜ ﺮرة أﻣﺎ ﻟﻠ ﺪور اﻷول‬ ‫ اﻟﻤﺤﺴ ﻮﺑﺔ ﻟﻠ ﺪور‬stiffness (K) ‫ﺘﺨﺪم‬

KFi xi 2 K ( x ) i Fi i=1

i=n

+

1 +

+

Fi % of each Frame = i = K n K Fi i=1

+

b

‫ﻮاﻧﯿﻦ اﻟﺴ‬

‫ﮭﯿﻞ ﻧﺴ‬

‫ اﻟﻤﺤﺴ ﻮﺑﺔ ﻣﻦ اﻟﻘ‬stiffness (K) -

‫و اﻷﺧ ﯿﺮ ﺗﻜ ﻮن ﻟﮭ ﺎ ﻗﯿ ﻢ آﺧﺮى و ﻟﻜ ﻦ ﻟﻠﺘﺴ‬

.(typical story)‫ﺮر‬

‫اﻟﻤﺘﻜ‬

For top story 24EI K int.= 3 c1 h

I b1

1 h Ic2 3I c1 2+ h ( Ibb1 + Ibb2 ) 1 2

24EI K ext.= 3 c2 2 + h

I b2 Ic2

Ic1 b1

1 3I c2 h ( Ibb1 ) 1

b2

‫ﻟﻠﻘ ﺮاءة ﻓﻘ ﻂ‬

For bottom story 24EI K int.= 3 c1 h

K ext.=

1 h Ic2 3I c1 2+ I h ( Ibb1 + Ibb2 ) h c2 1 2

24EI c2 2+ h3

- If I b >>> I c

Ib1

Ic1

Ib2

Ic2

Ic1 b1

b2

1 3I c2 h ( Ibb1 ) 1

The column considered as a fixed column K=

12EI c h3

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)

Ic2

Page No.


NOTE Symmetric

e *= 0.05 L

M T = Fb e* +

e min = 0.05 L

F1

F2

F2

F1

F1

F2

F2

F1

K1

K2

K2

K1

K1

K2

K2

K1

D.L.

T.L.

T.L.

T.L.

C.M.

D.L.

T.L.

C.M.

F1

F2

F2

F1

F1

F2

F2

F1

K1

K2

K2

K1

K1

K2

K2

K1

C.R.

emin x1

x2

C.R.

OR

C.M.

C.M.

= 0.05L

x2

x1

x1

Fb

e

min = 0.05L

x2

x2

x1

Fb

Fb +

KFi xi i=n 2 K ( x ) i Fi i=1

+

+

Fi Fi = i = K n K Fi i=1

+

‫ ( ﻛ ﺎﻵﺗﻲ‬frames ) ‫ ( ﻋﻠ ﻰ‬F b) ‫ﺛ ﻢ ﺗ ﻮزع اﻟﻘ ﻮة‬

MT

where: x i= (C.R.) ‫( ﻋﻦ‬frames)

‫ھﻮ ﺑﻌ ﺪ‬

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)

( 0.05 L Fb )

+

( 0.05 L Fb ) +

K2 2 ( K 1 + K2 )

+

F2 =

More Critical K1 x1 Fb + 2 2 2 [ K1( x 1) + K 2 (x 2) ] K2 x2 Fb + 2 2 2 [ K1( x 1) + K 2 (x 2) ]

+

K1 2 ( K 1 + K2 )

+

F1 =

+

e min

Page No.


Drift of structures due to seismic loads Importance of drift: Is to satisfy serviceability requirements. The drift should be limited to fulfill the safety requirements for non-structural elements. ‫ﻐﯿﻞ‬ ‫ﺎﺋﯿﺔ (واﺟﮭﺎت‬

‫ﻢ اﻟﻤﺴ ﻤﻮح ﺑﮭ ﺎ ﻃﺒﻘ ﺎً ﻟﺤ ﺪود اﻟﺘﺸ‬ ‫ﺎﻓﯿﺔ ﻋﻠ ﻰ اﻟﻌﻨﺎﺻ ﺮ اﻟﻐ ﯿﺮ إﻧﺸ‬

‫ﺄ ﻋﻦ اﻟﻘﯿ‬

‫ﺔ اﻟﺤﺎدﺛ ﺔ ﻟﻠﻤﻨﺸ‬

‫ﺒﺐ ﻓ ﻲ ﺗﻮﻟ ﺪ أﺣﻤﺎل إﺿ‬

‫ﯾﺠ ﺐ أﻻ ﺗﺰﯾ ﺪ اﻹزاﺣ ﺔ اﻟﻜﻠﯿ‬

‫اﻟﻤﻄﻠﻮﺑ ﺔ و ذﻟ ﻚ ﻟﻜ ﻲ ﻻ ﺗﺘﺴ‬

‫ ﺗ ﺆدي إﻟ ﻰ ﺗﺸ ﺮﺧﮭﺎ و اﻧﮭﯿﺎرھ ﺎ‬................) - ‫ ﺣ ﻮاﺋﻂ‬- ‫زﺟﺎج‬

Total Drift = Web Drift + Chord Drift

1- Web drift Shear ‫ﺔ‬

‫ﺄ ﻧﺘﯿﺠ‬

‫ﺔ ﺗﺤ ﺪث ﻟﻠﻤﻨﺸ‬

‫ھﻲ إزاﺣﺔ أﻓﻘﯿ‬

web drift D8

Q8 Q7

D7

Q6

D6 D5

Q5 Q4

D4

Q3

D3

Q2 Q1

Load diagram

Shear diagram

D2 D1

Drift diagram

Qi

+

+

% of each frame K Fi Total web drift for each frame ( SD i ) = S Q i % of each frame K Fi

Web drift for each frame ( D i ) =

where: Di = Story drift of each frame Q i = Shear force acting on the story C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


KFi xi 2 K ( x ) i Fi i=1

i=n

(1

+

K Fi 1 + K Fi i=1

i=n

+

(For Symmetrical Rigid Frames) +

% of each Frame =

K Fi K Fi i=1 i=n

+

% of each Frame =

e* )

(

For Unsymmetrical Rigid Frames

Case (a): Web drift for symmetrical rigid frames +

Web drift for each frame ( D i ) =

Qi

+

Qi

=

% of each frame K Fi K Fi K Fi i=1 i=n

=

K Fi

Qi i=n i=1

as K s =

i=n i=1

K Fi

K Fi

where K s = Story stiffness Q

Web drift ( D i) = Ki s Total web drift ( SD i) = ‫ﺎوﯾﺔ‬ D1

S Qi

‫ ﻣﺘﺴ‬frames ‫ﺔ ﻟﻜ ﻞ‬ D2

Ks ‫ﺔ ﺗﻜ ﻮن اﻹزاﺣ ﺔ اﻷﻓﻘﯿ‬ D2

‫ﻓ ﻲ ﺣﺎﻟ ﺔ اﻟﻤﻨﺸ ﺄت اﻟﻤﺘﻤﺎﺛﻠ‬

D1

Fb F1

F2

F2

F1

C.M. C.R.

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)

Page No.

)


Case (b): Web drift for unsymmetrical rigid frames Qi

+

+

% of each frame K Fi Total web drift for each frame ( SD i ) = S Q i % of each frame K Fi

Web drift for each frame ( D i ) =

‫ ﻋﻼﻗ ﺔ‬frames ‫ﺔ ﻟﻜ ﻞ‬

KFi xi 2 K ( x ) i Fi i=1

i=n

( 1 e* )

+

i=n

+

K Fi 1 + K Fi i=1

+

% of each Frame =

+

where:

‫ﺔ ﺗﻜ ﻮن اﻟﻌﻼﻗ ﺔ ﺑﯿ ﻦ اﻹزاﺣﺔ اﻷﻓﻘﯿ‬

( For Unsymmetrical rigid frames )

‫ﻓ ﻲ ﺣﺎﻟ ﺔ اﻟﻤﻨﺸ ﺄت اﻟﻐ ﯿﺮ ﻣﺘﻤﺎﺛﻠ‬ ‫ﺧﻄﯿ ﺔ‬

D1

D2 D3

straight line

F1

F2

D4

F3

F4

MT C.R.

C.M.

Fb

NOTE

H

ww KN/m

‫ ﻓﺄﻧ ﮫ ﯾﻤﻜ ﻦ‬wind load ( w ) ‫ ( ﻣﺜ ﻞ‬uniform load ) ‫ﻓ ﻲ ﺣﺎﻟ ﺔ ﺗﻌ ﺮض اﻟﻤﻨﺸ ﺄ إﻟ ﻰ‬ w ‫ ( ﻣﻦ اﻟﻤﻌﺎدﻟ ﺔ‬web drift ) ‫ﺣﺴ ﺎب‬ h

y(x) x

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2 y (x) = ww ( x H - 2x )

h Ks

)

Page No.


2- Chord drift Bending ‫ﺔ‬

‫ﺄ ﻧﺘﯿﺠ‬

‫ﺔ ﺗﺤ ﺪث ﻟﻠﻤﻨﺸ‬

‫ھﻲ إزاﺣﺔ أﻓﻘﯿ‬

H

we KN/m

Chord drift

Mbase Moment Diagram

B

we H Chord drift (D c) = 8EI e

Drift diagram

4

where: I e = Composite moment of inertia of columns at C.G. C.G

L2

L1

A1

A2

I1

I2 2

2

+

+

Ie = 2 [ I1 + A1 ( L1 ) ] + 2 [ I2 + A2 ( L 2 ) ] +

M Fi = % of each frame

M base = we H 2

2

get we

NOTE ‫ ﻟ ﺬﻟﻚ‬web drift ‫ﺒﺔ ﻟﻘﯿﻤ ﺔ‬

‫ ﻗﯿﻤ ﺔ ﺻ ﻐﯿﺮة ﺟ ﺪاً ﺑﺎﻟﻨﺴ‬chord drift ‫ﻏﺎﻟﺒ ﺎً ﻣﺎ ﺗﻜ ﻮن ﻗﯿﻤ ﺔ‬ ‫ﯾﻤﻜ ﻦ إھﻤﺎﻟﮭﺎ‬

DTotal = D web + D chord > D allowable =

H 500

600

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Page No.


Example. For the shown figure of a residential building lies at Aswan . The building consist of ( 8 ) repeated floors . L. L. = 2.0 kN/m 2& 2 F.C. = 1.5 kN/m and the soil is loose sand. Due to Earthquake loads , it is required to : 1- Calculate the story shear at each floor level and draw its distribution on the height of the building. 2- Find the bending moment and shearing forces acting at base level of the R.C. columns and draw distribution of shear force and bending moment. 3- Check Stability of the building against over turning Given that :

+

4 + 8=32 m

+

All beams = 25 60 All columns = 25 80 Slab thickness = 160 mm

Elevation

7 +3 = 21 m

+

7 3 = 21 m

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Page No.


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Fig. (8-1) P. (1/5 code)

Aswan

Loose sand

Table (8-2) P. (2/5 code)

Zone (2)

Table (8-1) P. (2/5 code)

a g = 0.125 g

Soil type (D)

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H

S = TB = TC = TD =

3/4

Beams + Columns

R.C. Frames

P. (5/5 code)

C t = 0.075

Total Height of building (H) = 32 m 3/4

+

T1 = 0.075 32 Check Sd (T)

= 1.01sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

Sd (T1 ) Time (Sec) TB TC

1.80 0.10 0.30 1.20

T1

TD

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4.0

)

Page No.


Eq. (8-13)

P. (3/5 code)

TC h > 0.20 a g g1 T1

Table (8-9) P. (4/5 code)

+

+

Sd (T1) = 0.125 g 1.00

g1 = 1.00 1.80

2.5 5.00

0.30 1.01

+

Sd (T1) = a g g1 S 2.5 R R = 5.00 h = 1.00

+

TC < T1 < TD

1.00

= 0.0334 g 0.20 a g g1 = 0.20

+

+

0.125 g 1.00 = 0.025 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

+

+

ws = D.L. + a L.L. ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code)

a = 0.25

+

+ +

+

+

+

+

+

+

+

+

+

ws = ( 0.16 25 + 1.5 ) + 0.25 2.0 = 6.0 kN/m2 beams columns slab wFloor = 6.0 21 21 + 0.25 0.6 25 ( 21 8) + 0.25 0.8 4 25 (16) = 3596 kN +

wTotal = 3596 8 = 28768 kN NOTE ts t av

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Page No.


l W g

+

= 0.0334 g

1.0

+

+

Fb = Sd (T1)

28768 g

F b = 960.85 kN

2- Distribution of lateral force on each floor +

Fi = Fb

w i Hi w i Hi i=1

i=n

w i Hi H = i=n i w i Hi i = 1 Hi i=1

i=n

‫ﻷن وزن اﻟ ﺪور ﺛﺎﺑ ﺖ‬

i=8

H = 32 + 28 + 24 + 20 +16 + 12 + 8 + 4 i i=1 = 144 m Fi = ( 960.85 ) 1 H i 144

28 20

Fi

=

16

6.6726 H i

12 4

Floor H (m) F (kN) Q (kN) i i i No. 32.0 213.52 213.52 8

8

Mi (kN.m) 854.09

7

28.0

186.83

400.35

2455.51

6

24.0

160.14

560.50

4697.49

5

20.0

133.45

693.95

7473.28

4

16.0

106.76

800.71

10676.11

3

12.0

80.07

880.78

14199.23

2

8.0

53.38

934.16

17935.87

1

4.0

26.69

960.85

21779.27

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)

Page No.

24

32


213.52

213.52

400.35

186.83

854.09

560.50

160.14

2455.51

693.95

133.45

800.71

106.76

26.69

7473.28

880.78

80.07 53.38

4697.49

10676.11

934.16

14199.23

960.85

17935.87 21779.27

Load Diagram

Shear Diagram

Moment Diagram

Shearing force at base = 960.85 kN Bending moment at base = 21779.27 kN.m

3- Check overturning Mbase U.L. = 21779.27 kN.m Mbase U.L. 21779.27 Moverturning = 1.40 = = 15556.62 kN.m 1.40 B 28768 2 =

+

+

Resisting Moment = WTotal

Resisting Moment

21 302064 kN.m 2 = 302064

Factor Of Safety = Over Turning Moment = 15556.62 = 19.4 > 1.5 Safe

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Page No.


Example. The shown figure of a building which lies at Cairo. The building consist of two basements, ground floor and mezzanine used as hospital and 8 repeated floors used as residential building.Live load and floor heights are shown in elevation, the average slab thickness 2 is 215 mm and Floor cover + walls = 2.5 kN/m . The soil is weak. Due to Earthquake loads , it is required to : 1- Calculate the equivalent seismic load acting on the building . 2- Draw lateral load ,shear and over turning moment diagram over the height of the structure. 2

L.L = 2.0 kN/m

2

L.L = 4.0 kN/m

2

2

L.L = 4.0 kN/m

2

L.L = 4.0 kN/m

2

6.0

L.L = 4.0 kN/m

2

L.L = 4.0 kN/m

6.0

3.0 +8 = 24 m

L.L = 4.0 kN/m

2

L.L = 4.0 kN/m

2

Void

6.0

2

L.L = 8.0 kN/m

6.0

2

L.L = 8.0 kN/m

2

L.L =10.0 kN/m

6.0

2

L.L =10.0 kN/m

6.0

6.0

6.0

6.0

6.0

Plan

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Sec . Elev

)

Page No.

3.5 3.5 4.0 4.0

L.L = 4.0 kN/m


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Fig. (8-1) P. (1/5 code)

Cairo

Table (8-1) P. (2/5 code)

Weak soil

Table (8-2) P. (2/5 code)

Zone (3)

a g= 0.15 g

Soil type (D)

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H Cores

S = TB = TC = TD =

3/4

C t = 0.05

P. (5/5 code)

Total Height of building (H) = 39 m 3/4

+

T1 = 0.05 39 Check

= 0.78sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

TC < T1 < TD

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R R = 5.00 h = 1.00

Eq. (8-13)

TC h > 0.20 a g g1 T1

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Page No.

1.80 0.10 0.30 1.20


Table (8-9) P. (4/5 code) Table (8-9) P. (4/5 code)

g1 = 1.40

g1 = 1.40 g1

1.80

+

+

Sd (T1) = 0.15 g 1.40

+

More critical

0.20 a g g1 = 0.20

0.30 0.78

2.5 5.00

+

NOTE

g1 = 1.00

1.00 = 0.0727 g

+

+

0.15 g 1.40 = 0.042 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

+

ws = D.L. + a L.L. +

ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code) Table (8-7) P. (5/5 code)

a = 0.25 a = 0.50 +

+

wfloor = ( D.L. + a L.L. ) area +

D.L. = t s gc + F.C. + Walls = ( 0.215 25 + 2.5) = 7.875 kN/m2 +

+

Area = 30 30 - 6.0 6.0 = 864 m2 void

+

+

+

wfloor = ( 7.875 + 0.25 2.0 ) 864 = 7236 kN +

Floor 12

+

+ +

wfloor = ( 7.875 + 0.50 10.0 ) 864 = 11124 kN Floor 2 & 3 wfloor = ( 7.875 + 0.50 8.0 ) 864 = 10260 kN Floor 4 11 wfloor = ( 7.875 + 0.25 4.0 ) 864 = 7668 kN +

Floor 1

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)

+

+

+

+

WTotal = ( 11124 1 + 10260 2 + 7668 8 + 6912 1 ) = 100224 kN Page No.


NOTE L.L. ~

l W g

+

= 0.0727 g

1.0

+

+

Fb = Sd (T1)

a

100224 g

F b = 7286.28 kN

2- Distribution of lateral force on each floor +

Fi = Fb

w i Hi w i Hi

i=n

i=1

Floor No. Hi (m) 12 39.0

wi (kN)

wi H i

Fi (kN)

Q i (kN)

Mi (kN.m)

7236

282204

993.30

993.30

2979.90

11

36.0

7668

276048

971.63

1964.93

8874.68

10

33.0

7668

253044

890.66

2855.59

17441.46

9

30.0

7668

230040

809.69

3665.28

28437.30

8

27.0

7668

207036

728.72

4394.01

41619.32

7

24.0

7668

184032

647.75

5041.76

56744.60

6

21.0

7668

161028

566.78

5608.54

73570.24

5

18.0

7668

138024

485.82

6094.36

91853.31

4

15.0

7668

115020

404.85

6499.21

117850.14

3

11.0

10260

112860

397.24

6896.45

145435.94

2

7.0

10260

71820

252.79

7149.24

170458.28

1

3.5

11124

38934

137.04

7286.28

195960.26

i=n i=1

w i Hi

i=n i=1

Fi

= 2070090 = 7286.28 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


993.30 1964.93 2855.59

12

993.30 971.63 890.66 809.69 728.72

11 10 9

3665.28 4394.01 5041.76

8

647.75

7 6

5608.54 6094.36

566.78 485.82

5

6499.21

404.85

4

6896.45

397.24

3

7149.24

252.79

2

7286.28

137.04

1

Load Diagram

Shear Diagram 2979.90 8874.68 17441.46 28437.30 41619.32 56744.60 73570.24 91853.31 117850.14 145435.94 170458.28

12 11 10 9 8 7 6 5 4 3 2 1

195960.26

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)

Page No.


Example. The shown figure of a student house which lies at Alexandria. The building consist of 15 repeated floors & Floor height = 3 m. The building consist of flat slab with average thickness 200 mm and shear walls 300 mm thickness .The soil is medium dense sand. It is required to : 1- Calculate the static wind load acting on the building in Y - direction and show its distribution over the height . 2- Calculate the equivalent seismic load acting in Y- direction. 3- Draw lateral load ,shear and over turning moment diagram over the height of the structure due to the critical lateral load .

4- Design the cross-section at the base of the Shear wall on axis 3 and draw its details of reinforcement . Given that : L.L. = 4.0 kN/m 2 1

2

3

6.0

4

4.0

6.0

12.0

Walls = 1.5 kN/m2

F.C. = 1.5 kN/m 2

6.0

5

4.0

6

6.0

6.0

6.0

Y

6.0

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)

Page No.


Solution 1- The static wind load Ce = 0.8 + 0.5 = 1.3

V = 36 m/sec

Alexandria 2

+

2

+ + +

1.00 0.81 = 1.053 kN/m 1.15 0.81 = 1.211 kN/m2 1.40 0.81 = 1.474 kN/m 2 1.60 0.81 = 1.685 kN/m2

+

q = 1.3 q = 1.3 q = 1.3 q = 1.3

+ + +

+

+

+

k1 k2 k3 k4

+

+

+

+

+

F4 = P4 ( h b) =1.685 15 30 = 758.25 kN

758.25 kN

1.685 kN/m

+

+

+

+

F3 = P3 ( h b) =1.474 10 30 = 442.20 kN

10 m

+

kN/m 37.5

+

F1 = P1 ( h b) =1.053 10 30 = 315.90 kN

1.211

363.30 kN

kN/m2

+

+

1.4742

442.20 kN

+

+

+

F2 = P2 ( h b) =1.211 10 30 = 363.30 kN +

15 m

2

10 m

25

Total wind force = 315.90 + 363.30

15

315.90 kN

+ 442.20 + 758.25

1.053 10 m 2

5

kN/m

= 751.86 kN

+

Fi H i

+

+

+

+

Total Moment at base ( Overturning Moment ) = = F1 H1 + F2 H2 + F3 H3 + F4 H4

+

+

+

+

= 315.90 5 + 363.30 15 + 442.20 25 + 758.25 37.5 = 46518.375 kN.m C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.

45 m

+

+

+

+

P1 = Ce P2 = Ce P3 = Ce P4 = Ce

+

+

+

+

-4 0.5 r V C t Cs 2 2 q= = 6.25 10 36 = 0.81 kN/m 1000 Zone A ( More Critical ) Pe = Ce k q (kN/m2 )


2- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Fig. (8-1) P. (1/5 code)

Alexandria

Table (8-1) P. (2/5 code)

Medium dense sand

Table (8-2) P. (2/5 code)

Zone (2)

Soil type (C)

Soil type (C) Table (8-3) P. (3/5 code)

Response spectrum curve Type (2)

T1 = Ct H

a g= 0.125 g

S = TB = TC = TD =

3/4

Shear walls

P. (5/5 code)

C t = 0.05

Total Height of building (H) = 45 m +

T1 = 0.05 Check

3/4

45

= 0.87sec.

T1 < ( 4 T C = 2.4 sec.) O.K. T1 < 2.0 sec.

TC < T1 < TD

O.K.

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R R = 5.00 h = 1.00 Table (8-9) P. (4/5 code)

Eq. (8-13)

TC h > 0.20 a g g1 T1

g1 = 1.00

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Page No.

1.25 0.20 0.60 2.00


0.60 0.87

2.5 5.00

+

1.25

+

+

+

Sd (T1) = 0.125 g 1.00

1.00

= 0.0539 g 0.20 a g g1 = 0.20

+

+

0.125 g 1.00 = 0.025 g < Sd (T1) O.K. T1 < 2 TC = 1.20 sec l = 0.85 P. (5/5 code)

+

+

ws = D.L. + a L.L. ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code)

a = 0.25 +

+

4.0 = 9.0 kN/m2

+

+

+

ws = ( 0.20 25 + 1.5 + 1.5 ) + 0.25 wFloor = 9.0 12 30 = 3240 kN wTotal = 3240 15 = 48600 kN

l W g

+

= 0.0539 g

0.85

+

+

Fb = Sd (T1)

48600 g

F b = 2226.61 kN

3- Distribution of lateral force on each floor +

Fi = Fb

w i Hi w i Hi i=1

i=n

w i Hi H = i=n i w i Hi i = 1 Hi i=1

i=n

‫ﻷن وزن اﻟ ﺪور ﺛﺎﺑ ﺖ‬

i = 15 i=1

H = 45 + 42 + 39 + 36 +33 + 30 + 27+ 24 + 21+ 18 + 15+ 12 + 9 + 6 i + 3 = 360 m C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


Fi Fi

1 H ) ( 2226.61 = 360 i

=

Floor H (m) F (kN) i i No. 15 45.0 278.33

6.185 H i

Moverturning =

Mbase U.L. 1.40

Q i (kN)

Mi (kN.m)

278.33

834.98

14

42.0

259.77

538.10

2449.27

13

39.0

241.22

779.31

4787.21

12

36.0

222.66

1001.97

7793.14

11

33.0

204.11

1206.08

11411.38

10

30.0

185.55

1391.63

15586.27

9

27.0

167.00

1558.63

20262.15

8

24.0

148.44

1707.07

25383.35

7

21.0

129.89

1836.95

30894.21

6

18.0

111.33

1948.28

36739.07

5

15.0

92.78

2041.06

42862.24

4

12.0

74.22

2115.28

49208.08

3

9.0

55.67

2170.94

55720.92

2

6.0

37.11

2208.05

62345.08

1

3.0

18.56

2226.61

69024.91

= 69024.91 = 49303.51 kN.m 1.40

Overturning Moment ( Seismic ) Overturning Moment ( wind )

= 49303.51 kN.m

= 46518.375 kN.m

The case of seismic load is the critical one

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Page No.


278.33 538.10 779.31 1001.97 1206.08 1391.63 1558.63 1707.07 1836.95 1948.28 2041.06 2115.28 2170.94 2208.05 2226.61

278.33

15 14 13 12 11 10 9 8 7 6 5 4 3 2 1

259.77 241.22 222.66 204.11 185.55 167.00 148.44 129.89 111.33 92.78 74.22 55.67 37.11 18.56

Load Diagram

Shear Diagram 15 834.98 14 2449.27 13 4787.21 12 7793.14 11 11411.38 10 15586.27 9 20262.15 8 25383.35 7 30894.21 6 36739.07 5 42862.24 4 49208.08 3 55720.92 2 62345.08 1 69024.91

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Page No.


4- Design of shear wall +

Isw2 =

3

0.30 ( 6.0 ) 12

1

2

4

= 5.40 m = Isw5

3

sw2

4

sw3

5

sw4

6

sw5

C.R.

3

+

Isw3 = 0.30 ( 4.0 ) = 1.60 m4 = Isw4 12 i=4 4 I = 2 ( 5.4 + 1.6 ) = 14.0 m

C.M.

e min

i=1

6.0

For Shear Walls on Axis 3

6.0

6.0

6.0

6.0

+

e min = 0.05 L = 0.05 30 = 1.5 m +

+

1.6 3.0 2 2 2 ( 1.6 3.0 + 5.4 9.0 )

1 1.5

+

+ +

+

1+

emin) +

+

1.6

= 2 ( 1.6 + 5.4 ) +

% of Sw3

Ii xi (1 2 I ( xi) i=1 i

i=n

+

+

% of each Shear Wall = i = In i 1 + Ii i=1

= 0.1223 = 12.23 %

Msw = % of Sw3 M base 3

+

3

+

= 0.01223 69024.91 = 8438.56 kN.m

+

ND.L. = g s

Area + o.w

+

By Area Method get the Normal force

8.0 4.0

No of floors

g s = ( t s gc + F.C. + Walls ) 2 ( 0.20 25 + 1.5 + 1.5 ) 8.0 kN/m = =

+

+

+

+

15 = 7110 kN

No of floors

(6.0 8.0 )

+

+

= 4.0

Area

+

+

NL.L = Ps

No of floors

(6.0 8.0 ) + (0.3 4.0 3.0 25 )

+

+

ND.L. = 8.0

Area + o.w

+

+

ND.L. = g s

+

+

6.0

15 = 2880 kN

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Page No.


Nult = 1.12 ND.L.+ a N L.L.+ N S.L. 7110 + 0.25 2880 + 0 = 8683.2 kN +

+

= 1.12

M ult = 1.12 M D.L.+ a M L.L.+ M S.L. = 0 + 8438.56 = 8438.56 kN.m

+

+

+ + + +

Nu = 8683.2 10 3 = 0.289 25 300 4000 Fcu b t 6 Mu 8438.56 10 0.0703 2 = 2 = 25 300 4000 Fcu b t Get

-4

Fcu 10 ) b t

+

+

+

+

-4

= 2.0 25 10

300 4000 = 6000 mm2

+

\

As = A s = (

= 2.0

+

x = 0.9

+

As = 0.6 Ac= 0.6 ( 300 4000 ) = 7200mm2 min 100 100 12

5

8/m

5

10 / m \

5

16 / m \

28

12

12 28

28 0.3

4.0

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Page No.


Example. For the given plan of a residential building, located in Hurghada (Seismic Zone 5A). The building consists of ground floor and 5 typical floors. The building is constructed on a weak soil. It is required to : 1- Calculate the shear base at ground floor level 2- Draw the lateral load & shear distribution diagrams 3- Calculate the seismic loads acting on the frame (F1)

Given that :

+

St. = 360/520 Fcu = 25 N/mm 2 F.C. + Partitions = 3.0 kN/m 2 t s av = 250 mm All columns are (300 800) The stiffness of exterior frames is twice the stiffness of interior frames 7.0 4.0 4.0 4.0 4.0

7.0

F2

F1

L.L. = 2.0 kN/m 2 L.L. = 2.0 kN/m 2 L.L. = 2.0 kN/m 2 L.L. = 7.0 kN/m 2 L.L. = 7.0 kN/m 2

8.0

F3

8.0

F4

6.0

8.0

4.0

7.0

L.L. = 2.0 kN/m 2

8.0

Sec . Elev

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8.0

)

Page No.


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Hurghada (Zone 5A) Weak soil

Table (8-2) P. (2/5 code)

Table (8-1) P. (2/5 code)

a g = 0.25 g

Soil type (D)

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H

S = TB = TC = TD =

3/4

Beams + Columns

R.C. Frames

P. (5/5 code)

C t = 0.075

Total Height of building (H) = 30 m 3/4

+

T1 = 0.075 30 Check

1.80 0.10 0.30 1.20

= 0.96 sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

TC < T1 < TD

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R R = 5.00 h = 1.00

Eq. (8-13)

TC h > 0.20 a g g1 T1

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Page No.


Table (8-9) P. (4/5 code)

2.5 5.00

0.30 0.96

+

1.80

+

+

+

Sd (T1) = 0.25 g 1.00

g1 = 1.00 1.00

= 0.0703 g 0.20 a g g1 = 0.20

+

+

0.25 g 1.00 = 0.050 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

+

+

ws = D.L. + a L.L. ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code)

a = 0.25 +

+

wfloor = ( D.L. + a L.L. ) area +

D.L. = t s gc + F.C. + Walls = ( 0.25 25 + 3.0) = 9.25 kN/m2 +

+

Area = 16 21 - 4.0 7.0 = 308 m2 void

6

wfloor = ( 9.25 + 0.25 7.0 ) 308 = 3388 kN wfloor = ( 9.25 + 0.25 2.0 ) 308 = 3003 kN +

3

2

+

Floor

&

+

1

+

Floor

+

+

WTotal = ( 3388 2 + 10260 4 ) = 18788 kN

l W g

+

= 0.0703 g

1.0

+

+

Fb = Sd (T1)

18788 g

F b = 1320.80 kN

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Page No.


2- Distribution of lateral force on each floor +

Fi = Fb Floor No. Hi (m) 6 30.0

w i Hi w i Hi i=1

i=n

wi (kN)

wi H i

Fi (kN)

Q i (kN)

3003

90090

327.96

327.96

5

26.0

3003

78078

284.23

612.19

4

22.0

3003

66066

240.50

852.69

3

18.0

3003

54054

196.77

1049.46

2

14.0

3388

47432

172.67

1222.13

1

8.0

3388

27104

98.67

1320.80

i=6 i=1

w i Hi

= 362824

327.96 612.19 852.69 1049.46 1222.13 1320.80

6 5 4 3 2 1

Shear Diagram

327.96 284.23 240.50 196.77 172.67 98.67

Load Diagram

3- Seismic loads acting on frame (F1) Plan is unsymmetric as C.M. = C.R. - C.R. is at the center of the plan as K is symmetric for frames ( K F1 = K F4 & K F2 = K F3 )

21

X C.R.= 2 = 10.5 m

- As the stiffness of exterior frames is twice the stiffness of interior frames ( K F1 = K F4 = 2 K F2 = 2 K F3 ) C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


7.0

14.0

4.0

Datum

A2 C.G.

12.0

A1

C.M.

C.G.

X C.M. 3.5 14.0

Ai x i Ai +

+

+

+

wi Ai x i = wi A i

X C.M.=

+

+ +

+

+

X C.M.= 7.0 12.0 3.5 + 14.0 16.0 14.0 = 11.14 m +

7.0 12.0 + 14.0 16.0

NOTE D.L. & L.L.

wi

( 1 e* )

+

KFi xi i=n 2 K ( x ) i Fi i=1

+

1 +

+

Fi % of each Frame = i = K n K Fi i=1

+

+

e = X C.M. - X C.R. = 11.14 - 10.5 = 0.64 m e * = e + 0.05 L = 0.64 + 0.05 21.0 = 1.69 m

K F1 = KF4 & KF2 = K F3 K F1 = 2 K F2 i=1

K Fi = 2 K F1 + 2 K F2 = 2 2 K F2 + 2 K F2 = 6 K F2 +

i=n

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Page No.


7.0

8.0

7.0

7.0

MT 0.64

C.R. C.M.

Zone (2)

Zone (1)

8.0

F1

3.5

+

+

+ +

1 1.69

+

1 1.69

+ +

+

2 K F2 10.5 2 2 2 ( 2 K F2 10.5 + K F2 3.5 ) +

1+

2 ( K F1

K F1 10.5 2 2 10.5 + K F2 3.5 )

+

2 K F2 6 K F2

‫ ﯾﻘ ﻊ ﻓ ﻲ‬frame ‫ﻷن‬

+

=

1+

zone (1)

+

K F1 6 K F2

+

% of F1 =

+

10.5

= 0.4096 = 40.96 % +

+

Fi = % F1 Fi = 0.4096 Fi

for F1

134.33 116.42 98.51 80.60 70.72 40.41

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Page No.


Example. The figure shows a residential building which lies at Aswan. It consist of 15 repeated floors & Floor height = 3 m. The building consist of prestressed slab with average thickness 200 mm and shear walls and cores 250 mm thickness .The soil is weak. It is required to : 1- Calculate the equivalent static load acting on the building at each floor and show its distribution over the height . 2- Determine the center of rigidity of the structure . 3- Compute the torsion moment at the ground level. 4- Calculate the percentage of lateral load acting on each shear wall and core.

Given that : L.L. = 6.0 kN/m 2 1

Walls = 1.5 kN/m2

F.C. = 1.5 kN/m 2

2

3

4

5

6

A 5.0

B 5.0

C 5.0

D 5.0

E 6.0

6.0

6.0

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6.0

)

6.0 Page No.


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Fig. (8-1) P. (1/5 code)

Aswan

Weak soil

Table (8-2) P. (2/5 code)

Zone (2)

Table (8-1) P. (2/5 code)

a g = 0.125 g

Soil type (D)

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H

S = TB = TC = TD =

3/4

Shear walls + Cores

C t = 0.05

P. (5/5 code)

Total Height of building (H) = 45 m

Check

3/4

+

T1 = 0.05

45

= 0.87sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

TC < T1 < TD

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R R = 5.00 Prestressed concrete

Eq. (8-13)

TC h > 0.20 a g g1 T1 Table (8-4) P. (3/5 code)

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h = 1.05 )

Page No.

1.80 0.10 0.30 1.20


Table (8-9) P. (4/5 code)

0.30 0.87

2.5 5.00

+

1.80

+

+

+

Sd (T1) = 0.125 g 1.00

g1 = 1.00 1.05

= 0.0407 g 0.20 a g g1 = 0.20

+

+

0.125 g 1.00 = 0.025 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

+

+

ws = D.L. + a L.L. ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code)

a = 0.25 +

+

ws = ( 0.20 25 + 1.5 + 1.5 ) + 0.25

6.0 = 9.5 kN/m2

+

+

Fb = Sd (T1)

l W g

+

= 0.0407 g

1.0

+

+ +

wFloor = 9.5 20 30 = 5700 kN wTotal = 5700 15 = 85500 kN

85500 g

F b = 3479.85 kN

2- Distribution of lateral force on each floor +

Fi = Fb

w i Hi w i Hi i=1

i=n

w i Hi H = i=n i w i Hi i = 1 Hi i=1

i=n

‫ﻷن وزن اﻟ ﺪور ﺛﺎﺑ ﺖ‬

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Page No.


Floor H (m) i No.

i = 15

H = 45 + 42 + 39 + 36 +33 + 30 + 27 i + 24 + 21+ 18 + 15+ 12 + 9 + 6 + 3 = 360 m

i=1

Fi

Fi

Fi (kN)

15

45.0

434.98

14

42.0

405.98

13

39.0

376.98

=

1 H ( 3479.85) 360 i

12

36.0

347.99

11

33.0

318.99

=

9.666 H i

10

30.0

289.99

9

27.0

260.99

8

24.0

231.99

7

21.0

202.99

6

18.0

173.99

5

15.0

144.99

4

12.0

116.00

3

9.0

87.00

2

6.0

58.00

1

3.0

29.00

434.98 405.98 376.98 347.99 318.99 289.99 260.99 231.99 202.99 173.99 144.99 116.00 87.00 58.00 29.00

Load Diagram

3- Center of rigidity and torsional moment 1

For Shear walls

3

4

5

6

a

3

5.0

+

Ix = 0.25 10.0

2

b

12

5.0

C.R.

4

= 20.83 m

c

x

10.0

C.M.

x

5.0

d 5.0

e 6.0

6.0

6.0

6.0

0.25 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.

6.0


For Core

y

x 5.0

+

+ +

+

+ + +

+

y = 4.75 0.25 2 2.625 + 6.0 0.25 0.125 4.75 0.25 2 + 6.0 0.25

0.25

= 1.66 m

6.0

( 2.625 - 1.66 )

3

2

2

4

+

+

+

20.83 0 + 20.83 6 + 10.22 21 + 20.83 30 20.83 3 + 10.22 + +

+

+

+ 0.25 6.0 ( 1.66 - 0.125 ) = 10.22 m

Ii xi = Ii

X C.R.=

+

+

+ 0.25 4.75

+

+ 6.0 0.25 12

2

+

+

3

+

0.25 4.75 12

Ix =

x

= 13.26 m

X C.M.= L = 30 =15.0 m 2 2

+

e = X C.M. - X C.R. = 15.0 - 13.26 = 1.74 m e * = e + 0.05 L = 1.74 + 0.05 30.0 = 3.24 m 4- Percentage of lateral load carried by shear walls & cores

1

2

3

4

5

+

+

i=n

+

Ii xi (1 2 I ( x i) i=1 i

% of each Shear Wall = i = nI i 1 + Ii i=1

e* )

6

a

5.0 b

5.0

C.R. c

C.M.

5.0

d

(+ ve) Zone (1)

(- ve) Zone (2)

5.0

e

6.0

6.0

6.0

6.0

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6.0

)

Page No.


+

+

20.83 13.26 2 2 2 2 20.83 (13.26 + 7.26 + 16.74 ) + 10.22 7.74 +

+

1 - ( 1 3.24 )

+

F 1 =20.8320.83 3 + 10.22

+

For Shear Walls on Axis 1

= 20.66 %

+

20.83 7.26 2 2 2 20.83 (13.26 + 7.26 + 16.74 ) + 10.22 7.74 +

2

+

+

1 - ( 1 3.24 )

+

F 2 =20.8320.83 3 + 10.22

+

For Shear Walls on Axis 2

= 24.28 %

+

20.83 16.74 2 2 2 20.83 (13.26 + 7.26 + 16.74 ) + 10.22 7.74

1 + (1 3.24 )

10.22 7.74 2 2 2 20.83 (13.26 + 7.26 + 16.74 ) + 10.22 7.74

+

+

1 + ( 1 3.24 )

+

2

+

+

F 3 =20.8320.83 3 + 10.22

+

For Shear Walls on Axis 6

= 38.73 % +

+

2

+

+

F4 =20.8310.22 3 + 10.22

+

For Core

= 16.34 %

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)

Page No.


Example. The shown figure of a residential building which lies at Cairo . It consist of a ground, mezzanine and 8 repeated floors and two basements. Live load and floor heights are shown in elevation. The soil below the building is weak. Due to Earthquake loads , it is required to : 1- Calculate the story shear at each floor level . 2- Calculate the total lateral drift . 3- Draw the distribution of web drift along the height of the building . Given that : F.C. = 1.5 kN/m 2

Slab thickness = 160 mm All Beams are ( 300 600 ) All Column are ( 300 700 ) +

+

2 E = 22100 N/mm L.L = 2.0 kN/m 2 L.L = 4.0 kN/m 2 L.L = 4.0 kN/m 2

+

5

6 m =30m

L.L = 4.0 kN/m 2

4+ 6m =24 m

L.L = 4.0 kN/m 2 L.L = 4.0 kN/m 2 L.L = 4.0 kN/m 2 L.L = 4.0 kN/m 2 L.L = 8.0 kN/m

2

L.L = 8.0 kN/m 2

Plan

L.L = 10.0 kN/m 2 L.L = 10.0 kN/m 2

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Page No.

3.0 +12 = 36 m

L.L = 4.0 kN/m 2


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location Fig. (8-1) P. (1/5 code)

Aswan

Table (8-1) P. (2/5 code)

Loose sand

Table (8-2) P. (2/5 code)

Zone (2)

a g = 0.125 g

Soil type (D)

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H

S = TB = TC = TD =

3/4

Beams + Columns

R.C. Frames

P. (5/5 code)

C t = 0.075

Total Height of building (H) = 36 m 3/4

+

T1 = 0.075 36 Check

1.80 0.10 0.30 1.20

= 1.10sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

TC < T1 < TD

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R

Eq. (8-13)

TC h > 0.20 a g g1 T1

R = 5.00 h = 1.00 Table (8-9) P. (4/5 code)

g1 = 1.00

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2.5 5.00

0.30 1.10

+

1.80

+

+

+

Sd (T1) = 0.125 g 1.00

1.00

= 0.0307 g 0.20 a g g1 = 0.20

+

+

0.125 g 1.00 = 0.025 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

+

+

ws = D.L. + a L.L. ws = ( t s gc + F.C. + Walls ) + a L.L. Table (8-7) P. (5/5 code)

a = 0.25

+

+

+

+

+

+

+

+

+

+

4

+

3.0 = 6520.50 kN

+

24 30 + 0.3 0.6 25 ( 24 6 )

wFloor = ( 5.5 + 0.25 8.0 ) + 0.3 0.7 25 30 Floor

+

+

+

+

C.L.-C.L.

3

+

&

+

2

+

Floor

+

+

+

+

ws = ( 0.16 25 + 1.5 ) = 5.5 kN/m2 Floor 1 beams slab wFloor = ( 5.5 + 0.25 10.0 ) 24 30 + 0.3 0.6 25 ( 24 6) columns + 0.3 0.7 25 30 4.5 = 7116.75 kN NOTE

11

+

+

+

+

+

+

+

+

+

+

+

wFloor = ( 5.5 + 0.25 4.0 ) 24 30 + 0.3 0.6 25 ( 24 6) + 0.3 0.7 25 30 3.0 = 5800.5 kN

+

)

+

+

+

+

+

+

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+

1.5 = 5204.25 kN

wFloor = ( 5.5 + 0.25 2.0 ) + 0.3 0.7 25 30

+

+

24 30 + 0.3 0.6 25 ( 24 6)

+

Floor 12

Page No.


+

+

l W g

+

= 0.307 g

1.0

+

+

Fb = Sd (T1)

+

+

WTotal = ( 7116.75 1 + 6520.50 2 + 5800.50 8 + 5204.25 1 ) = 71766 kN

71766 g

F b = 2203.22 kN

2- Distribution of lateral force on each floor +

Fi = Fb

Floor No. Hi (m) wi (kN) 36.0 5204.25 12

w i Hi w i Hi i=1

i=n

wi H i

Fi (kN)

Fi H i (kN.m)

187353.00

305.63

11002.57

11

33.0

5800.50

191416.50

312.26

10304.44

10

30.0

5800.50

174015.00

283.87

8516.06

9

27.0

5800.50

156613.50

255.48

6898.01

8

24.0

5800.50

139212.00

227.09

5450.28

7

21.0

5800.50

121810.50

198.71

4172.87

6

18.0

5800.50

104409.00

170.32

3065.78

5

15.0

5800.50

87007.50

141.93

2129.02

4

12.0

5800.50

69606.00

113.55

1362.57

3

9.0

6520.50

58684.50

95.73

861.58

2

6.0

6520.50

39123.00

63.82

382.93

1

3.0

7116.75

21350.25

34.83

104.49

i = 12

i = 12

w i Hi i=1

i=1

= 1350600.75 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

Fi H i = 54250.59

)

Page No.


3- Total drift Chord Drift Fi H i = 54250.59 kN.m

M over turning = 2

= 54250.59 = w 36

2

w = 83.72 kN/m

+

M =wH 2

2

3

+

Ic = 0.3 0.7 = 0.0086 m4 12

12.0

( I c + A 12 2 ) +

+

( Ic + A 6 2 ) + 2 +

[ Ic + 2

+

Ie = 6

6.0

] +

+

+

+

+

+

2 2 = 6 [0.0086 + 2 (0.0086 + 0.3 0.7 6 ) + 2 (0.0086 + 0.3 0.7 12 )]

4 = 453.86 m 4

4

= 0.00175 m

+

+

+

+

wH = 83.72 36 Chord drift (Dc) = 8EI 8 2.21 10 7 453.86 e

= 1.75 mm Web Drift Assume ( K ) constant for all floors Typical Story 3

+

4 Ic = 0.3 0.7 = 0.0086 m 12 3

+

4 Ib1= Ib2 = 0.3 0.6 = 0.0054 m 12

12EI c1 h3

7

1 2 0.0086 1+ 3 (0.0054 +0.0054 ) 6.0 6.0

= 20183.4 kN/m

+

( 3.0 )3

+

+

+

K int.=

12 2.21 10 0.0086

+

K int.=

1 2I c1 1+ h ( Ibb1 + Ibb2 ) 1 2

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Page No.


1 2I c2 h ( Ibb1 ) 1

12EI c2 1+ h3

K ext.=

7

+

+

+

3

+

( 3.0 )

= 11460.9 kN/m

+

=

1 2 0.0086 1+ 3 (0.0054 ) 6.0

12 2.21 10 0.0086

K = SK

+int. SK

F1

ext. = 3 K int. + 2 K ext.

i=6 i=1

K Fi = 6 K F1 = 6 83472 = 500832 kN/m +

Ks =

+

+

= 3 20183.4 + 2 11460.9 = 83472 kN/m Floor No. Hi (m) 12 36.0

S Qi

Fi (kN)

Q i (kN)

Qi

305.63

305.63

18083.53

36.11

Di =

Ks

(mm) 36.11 35.50

11

33.0

312.26

617.88

17777.90

35.50

10

30.0

283.87

901.75

17160.02

34.26

9

27.0

255.48

1157.23

16258.27

32.46

8

24.0

227.09

1384.33

15101.03

30.15

7

21.0

198.71

1583.04

13716.71

27.39

6

18.0

170.32

1753.36

12133.67

24.23

20.73

5

15.0

141.93

1895.29

10380.31

20.73

16.94

4

12.0

113.55

2008.84

8485.02

16.94

3

9.0

95.73

2104.57

6476.18

12.93

2

6.0

63.82

2168.39

4371.61

8.73

1

3.0

34.83

2203.22

2203.22

4.40

i = 12 i=1

Qi

= 18083.53

Total web drift ( SD i) =

S Qi Ks

34.26 32.46 30.15 27.39 24.23

12.93 8.73 4.40

Web Drift Diagram

18083.53

= 500832 = 0.03611 m = 36.11 mm

Total Drift = Web Drift + Chord Drift = 36.11 + 1.75 = 37.86 mm. C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

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Page No.


Example. The given figures show sectional elevation and cross sections of a minaret of 51.4 meters height constructed in Sharm El Sheikh above loose soil. The thickness of minaret walls is 400 mm up to level 33.4 m supporting 8 circular posts of 300 mm diameter. The rest of the minaret is a cylindrical wall of 300 mm thickness covered by a cone of 3.0 height. The minaret is supported on shallow foundation,where top of footing is at 2.0 meter depth below ground. It is required to : 1- Calculate the equivalent base shear acting on the minaret. 2- Determine the overturning moment of the minaret. 3- Calculate the breadth of the minaret footing to ensure proper safety against over turning.

Given that : - No. L.L. or F.C. will be considered in calculations - A steel stair is used inside the minaret, its weight will be neglected. - Foundation depth is 1.0 m. (Take foundation weight into consideration in stability calculations). - Surface area of the cone is as follows

Surface Area =

L r +

L

+

h

C.G.

r

h/3

Cone

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Page No.


0.40

3.00

3.00

0.40

4.00

8.00

4.00

SEC. (A-A)

E

E

D

D 4.00

C

C

B

B 10.00

A

A

0.

40

1.66

8.00

4.00

0.40

0.40

2.60 0.3 0

1.66 4.00

SEC. (B-B)

6.00 2.49

1.76

SEC. (E-E)

1.76

1.66 1.76 0.

40

40

0.

1.90

Circular Posts 300mm

1.08

1.08

2.49

1.90

0.91

1.08

0.30

1.08

15.00

0.91

1.76

SEC. (D-D) SEC. (C-C)

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Page No.


Solution 1- Simplified Modal Response Spectrum

+

Fb = Sd (T1)

l W g

According to Soil type and building location (8-1) Sharm El Sheikh P.Fig. (1/5 code) Table (8-1) P. (2/5 code)

Loose soil

(8-2) Zone (5B) P.Table (2/5 code)

Soil type (D) S = TB = TC = TD =

Soil type (D) Table (8-3) P. (3/5 code)

Response spectrum curve Type (1)

T1 = Ct H

a g = 0.30 g

1.80 0.10 0.30 1.20

3/4

R.C. Core

C t = 0.05

P. (5/5 code)

Total height of minaret from foundation (H) = 50.4 m

Check

3/4

+

T1 = 0.05

50.4

= 0.946 sec.

T1 < ( 4 T C = 1.2 sec.)

O.K.

T1 < 2.0 sec.

O.K.

TC < T1 < TD

P. (3/5 code)

Sd (T1) = a g g1 S 2.5 R Table (A) P. (4/5 code)

51.4 50.4

48.4

Eq. (8-13)

TC h > 0.20 a g g1 T1 2.0

R = 3.50

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Page No.


Table (8-4) P. (3/5 code)

Reinforced concrete

1.80

+

1.20

2.5 3.50

0.30 0.946

+

g1 = 1.20 +

Sd (T1) = 0.30 g

+

Table (8-9) P. (4/5 code)

h = 1.00

1.00

= 0.1468 g 0.20 a g g1 = 0.20

+

+

0.30 g 1.20 = 0.072 g < Sd (T1) O.K. T1 > 2 TC = 0.60 sec l = 1.00 P. (5/5 code)

Calculation of Minaret weight Part (7)

Part (1)

2.94

+ +

Part (5)

7.84

3.92

Part (4)

+

+

+

+

+

+ + + + +

+

Volume Density Weight = = ( Surface Area Thickness ) Density = ( Perimeter h Thickness ) Density = ( Perimeter h t w ) gc = 4 4.0 17.0 0.40 25 = 2720 kN

Part (6)

4.0

7.84 0.39 50.4

Part (2)

0 .4 0

9.80

0.39

4.0

Part (3)

0.40

3.92

17.0

Part (1) 17.0

2.0

3.92

SEC. (A-A) C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

)

Page No.


1.62 39

+

0.

+

+ + +

+

+

Part (2) ( h = 10.0 m ) Weight = ( Perimeter h t w ) gc = 8 1.66 10.0 0.40 25 = 1328 kN

3.92

0.40 1.62 3.92

SEC. (B-B)

1.72

2.44

1.72

+

+

Part (3) ( Horizontal slab t s = 0.40 m ) Weight = ( Area t s ) gc

2

+

+

+

+

+ 2.49 ) 1.9 0.40 25 ( 0.912.0 1 8 = 258.4 kN 1.86 =8

2.44

3 1.86

4

0.89 0.89

7

6

5

SEC. (C-C)

+

1.06

+

+ + +

+

39

+

1.06

0.

Part (4) ( h = 8.0 m ) Weight = ( Perimeter h t w ) gc = 8 1.08 8.0 0.40 25 = 691.2 kN

SEC. (D-D)

0.29

+

+ +

Part (5) ( h = 4.0 m ) Weight = ( Area h No. of posts ) gc 2

0.3 4

+

+

+

+

4.0 8.0 25 = = 226.2 kN C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

Circular Posts 300mm

SEC. (D-D)

)

Page No.


+

2.60 0.3 0

+

+ + +

+

+

Part (6) ( h = 8.0 m ) Weight = ( Perimeter h t w ) gc 2.60 8.0 0.30 25 = = 490.1 kN

SEC. (E-E)

Part (7) 3.354

3.0

+

+

Surface Area = (Given)

3.0

L

L r h +

+

+

Volume Density Weight = = ( Surface Area Thickness ) Density

r

Cone

+

+ +

+

+ +

+ + +

+

+

+

L r Thickness ) Density =( L r Thickness ) Density = 3.354 1.50 0.30 25 = = 118.5 kN WTotal = WParts WTotal = 2720 + 1328 + 258.4 + 691.2 + 226.2 + 490.1 + 118.5 WTotal = 5832.4 kN

+

= 0.1468 g

l W g 1.0

+

+

Fb = Sd (T1)

5832.4 g

F b = 856.2 kN

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)

Page No.


2- Distribution of lateral force on each part Part (7)

+

Fi = Fb

2.94

Part (6)

W6

7.84

Part (5)

W5

3.92

Part (4)

W7

w i Hi w i Hi

i=n

i=1

Check Overturning

W4

Part (3) 7.84

48.4

W2

43.4

Overturning Moment

Part (2)

0.39 50.4

W3

9.80

37.4 31.4 27.2

Part (1)

22.0

W1

17.0 8.5 2.0

(Given) 1.0 Overturning Point

B

Part No. 7

Hi (m)

wi (kN)

wi H i

48.4

118.5

5735.4

42.14

49.4

2081.68

6

43.4

490.1

21270.34

156.28

44.4

6938.74

5

37.4

226.2

8459.88

62.16

38.4

2386.82

4

31.4

691.2

21703.68

159.46

32.4

5166.56

3

27.2

258.4

7028.48

51.64

28.2

1456.24

2

22.0

1328

29216

214.66

23.0

4937.10

1

8.5

2720

23120 w i Hi

169.87

9.5

1613.74

i=7 i=1

Fi (kN) Hbase (m)

i=7 i=1

= 116533.78 C Copyright . All copyrights reserved. Downloading or printing of these notes is allowed for personal use only. ( Commercial use of these notes is not allowed.

Fi H i (kN.m)

Fi Hbase = 24580.89

)

Page No.


3- Check overturning Mbase U.L. = 24580.89 kN.m Mbase U.L. 24580.89 Moverturning = 1.40 = 1.40 = 17557.78 kN.m +

Footing Dimensions = B B 0.40

+

+

+

Footing Weight = B B 1.0 25 2 = 25 B 2 WTotal = 25 B + 5832.4

0.40

4.00

4.00

+

Resisting Moment = WTotal

B 2

B +

2 ( 25 B + 5832.4 ) 2B = 3 12.5 B + 2916.2 B =

Resisting Moment Factor Of Safety = Over Turning Moment 3

1.50 =

12.5 B + 2916.2 B 24580.89

B = 9.25 m

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)

Page No.

B


NOTE Overturning Moment Soil Stresses Counter Weight

OR

Filling Material (Plain Concrete) as counter weight

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