Design of Wingwall

8/19/2019 Design of Wingwall

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DESIGN OF WINGWALL

File Name: marrrrrrrrrrrrrrrrrrrrr

I. Load Analysis

A. Geometry: detalye

1.15 m

2.50 m

0.25 m

2.50 m

0.15 m

0.80 m

0.66 m

Area

Wingwall 1: Wingwall 2: Wingwall 3:

Area = 2.88 Area = 2.94 Area =

1.25 m 0.9333 m

3.5938 2.41

!otal Area = 6.19

1.03 m

Weig"t

#on$rete %nit Weig"t: 24.0

Wingwall 1: Wingwall 2:

&ol'me = 2.300 &ol'me = 2.350

Weig"t = 55.200 (N Weig"t = 56.400 (N

)ara*et:

Area = 0.20

&ol'me = 0.50

Weig"t = 12 (N

+. ,art" )re--'re

1:

2:

3:

/1:

/2:

aim'n !"i$(ne-- !1:

inim'm !"i$(ne-- !2:

m2 m2

1 = 2 = 3 =

Area1 = m3 Area2 = m3 Area3

m2

/=

(Nm3

m3 m3

m2

m3


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)arameter-19.00

35.00 deg

ei-mi$ A$$eleration #oei$ient A: 0.40

0.60 7ta(en a- 1.5 o A

#"e$( or oriontal A$$eleration $oei$ient: (" 71;( 7AA!? #6.3.2 1

0.600 @ 0.00 o(

0.00

0.00 deg

B: 30.96 deg 7B = ar$ tan 7 (" 1 ; (<

Angle o Fri$tion Cetween oil and AD'tment E: 15.00 deg

Ca$(ill lo*e Angle >: 0.00 deg

%nit Weig"t o oil s: (Nm3

Fri$tion Angle :

oriontal A$$eleration #oei$ient ( ":

&erti$al A$$eleration #oei$ient (


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90.00 deg

ei-mi$ ,art" )re--'re 7ononoDe;?(aDe )rin$i*le

H

I = 1J = 1.6346

= 1.021

tati$ A$ti


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#a-e A = 1.3 O +/ J 2.2 // P 83.31 85.68

#a-e C = 1.3 O +/ J // J 1.3,P 114.2 108.2

#a-e = 1.3 O +/ J 1.3, P 6.40 69.33

#a-e & = 1.3 O +/ J 1.3, J ,M P 426.44 493.62

+e-ign oment: 135.24 (N;m+e-ign "ear: 116.83 (N


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0.38

0.05 m

0.0281

Wingwall 3:

&ol'me = 0.300

Weig"t = .200 (N

m2

= m3

m3


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A


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9/29

DESIGN OF WINGWALL

File Name: marrrrrrrrrrrrrrrrrrrrr

I. Load Analysis

A. Geometry: detalye

1.40 m 6.30

4.90 m

0.00 m

.0 m

0.00 m

0.45 m

0.80 m

Area

Wingwall 1: Wingwall 2: Wingwall 3:

Area = 10.8 Area = 18.8 Area =

3.85 m 2.566 m

41.503 48.42

!otal Area = 29.65

3.03 m

Weig"t

#on$rete %nit Weig"t: 24.0

Wingwall 1: Wingwall 2:

&ol'me = 4.851 &ol'me = 15.092

Weig"t = 116.424 (N Weig"t = 362.208 (N

)ara*et:

Area = 0.20

&ol'me = 1.54

Weig"t = 36.96 (N

+. ,art" )re--'re

1:

2:

3:

/1:

/2:

!"i$(ne-- !1:

!"i$(ne-- !2:

m2 m2

1 = 2 = 3 =

Area1 = m3 Area2 = m3 Area3

m2

/=

(Nm3

m3 m3

m2

m3


10/29

)arameter-18.80

35.00 deg

ei-mi$ A$$eleration #oei$ient A: 0.40

0.60 7ta(en a- 1.5 o A

#"e$( or oriontal A$$eleration $oei$ient: (" 71;( 7AA!? #6.3.2 1

0.600 @ 0.00 o(

0.00

0.00 deg

B: 30.96 deg 7B = ar$ tan 7 (" 1 ; (<

Angle o Fri$tion Cetween oil and AD'tment E: 15.00 deg

Ca$(ill lo*e Angle >: 0.00 deg90.00 deg

%nit Weig"t o oil s: (Nm3

Fri$tion Angle :

oriontal A$$eleration #oei$ient ( ":

&erti$al A$$eleration #oei$ient (


11/29

ei-mi$ ,art" )re--'re 7ononoDe;?(aDe )rin$i*le

H

I = 1J = 1.6346

= 1.021

tati$ A$ti


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#a-e A = 1.3 O +/ J 2.2 // P 394.93 119.94

#a-e C = 1.3 O +/ J // J 1.3,P 810.66 2240.69

#a-e = 1.3 O +/ J 1.3, P 631.15 1696.18

#a-e & = 1.3 O +/ J 1.3, J ,M P 3048.32 9518.38

+e-ign oment: 1510.9 (N;m+e-ign "ear: 483.86 (N


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0.00

0 m

0

Wingwall 3:

&ol'me = 0.000

Weig"t = 0.000 (N

m2

= m3

m3


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A


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TIC ACTIVE EARTH

29.345

98 26.92848 24.901

98 22.83

48 20.845

98 18.81

48 16.9098 14.6248 12.3498 10.0648 8.69

98 6.65148 4.62318 0.000

SEISMIC EARTH

0.00098 .54648 13.898 20.20

48 26.53898 32.86848 39.19998 45.52948 51.860 6.4898 58.190 11.5248 64.521 TTT98 0.851 2.618248 .18218 91.615


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II. Design of Reinforcement for Upper Sla !orners

A. e$tion )ro*ertie-

2.60 )a

414.00 )a

0.050 m

25 mm0 mm

emDer !"i$(ne-- " = 0.80 m

emDer Widt" D = 1.00 m

,e$ti


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#. +e-ign or "ear Keinor$ement

34 (N

6.00 (N ;m

o(ey

0.00444

trengt" Ked'$tion Fa$tor = 0.85

#on$rete "ear trengt"

but shall not exceed 713U7V$ Dd

and not be taken less than 714 U7V$ Dd

968.62 (N

Y 823.333 (N

' Stirr(ps are not needed

;528.62 (No(ey

10 mm

9

N'mDer o !ie- *er e$tion n = 3.333 *$-

*a$ing - =

- = ;151.195 mm

aim'm *a$ing:

&-

-ma = 368.5 mm

Ado*ted:

%& mm diameter ars $ )&&.&) per section $ %#& mm

+. "rin(age and !em*erat're Keinor$ement

0.403

o(ey402.56 mm2mm

12280.93 mm

aim'm *a$ing = 450 mm

Ado*ted:

%" mm diameter ars $ "#& mm

"ear at e$tion &+1 =

oment at e$tion +1 =

&+1d +1 ≤ 1

teel Katio )ro


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7AA!? 8.22.1

7AA!? 8.16.1.2.2

7AA!? 8.16.2.

7AA!? 8.15.2.1.1

7AA!? 8.13.3

7AA!? 8.1.1.1

7AA!? 8.16.4.2.3

7AA!? 8.16.3.1.1

345

mm2


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7AA!? 8.16.6..1

7AA!? 8.16.1.2.2

7AA!? 8.16.6..1

7AA!? 8.16.6.1.1

7AA!? 8.16.6.3.9

7AA!? 8.16.6.3.8

7AA!? /KF+ 200 ;

5.10.8


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II. Design of *ertical Reinforcement

A. e$tion )ro*ertie-

2.60 )a

414.00 )a

0.050 m

20 mmWall !"i$(ne-- " = 0.80 m

emDer Widt" D = 1.00 m

,e$ti


24/29

#. +e-ign or "ear Keinor$ement

34 (N

613.00 (N ;m

o(ey

0.00425

trengt" Ked'$tion Fa$tor = 0.85

#on$rete "ear trengt"

but shall not exceed 713U7V$ Dd

and not be taken less than 714 U7V$ Dd

91.910 (N

Y 826.124 (N

' Stirr(ps are not needed

;531.910 (No(ey

10 mm

9

N'mDer o !ie- *er e$tion n = 3.333 *$-

*a$ing - =

- = ;150.1 mm

aim'm *a$ing:

&-

-ma = 30 mm

Ado*ted:

%& mm diameter ars $ )&&.&) per section $ %#& mm

+. "rin(age and !em*erat're Keinor$ement

0.403

o(ey402.56 mm2mm

12280.93 mm

aim'm *a$ing = 450 mm

Ado*ted:

%" mm diameter ars $ "#& mm

"ear at e$tion &+1 =

oment at e$tion +1 =

&+1d +1 ≤ 1

teel Katio )ro


25/29


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7AA!? 8.22.1

7AA!? 8.16.1.2.2

7AA!? 8.16.2.

7AA!? 8.15.2.1.1

7AA!? 8.13.3

7AA!? 8.1.1.1

7AA!? 8.16.4.2.3

7AA!? 8.16.3.1.1

309

mm2


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7AA!? 8.16.6..1

7AA!? 8.16.1.2.2

7AA!? 8.16.6..1

7AA!? 8.16.6.1.1

7AA!? 8.16.6.3.9

7AA!? 8.16.6.3.8

7AA!? /KF+ 200 ;

5.10.8


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ea#th seismic

1"1$% &%'(%

)"! %%*) &%'(%

)(% &(1( (%)'1

)& ""'$ %'"(!

)& 1)1!1 !*%*%)& 1!("& !!)(&

)& 1($!* 1('*"

)& 1"1$% "%($

%'&

Date post:	08-Jul-2018
Category:	Documents
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Design of Wingwall

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