2. Bond
Basic assumptions in Flexural theory
Strain in concrete is the same as in reinforcing
bars at the same level, provided that the bond between
the steel and concrete is sufficient to keep them acting
together under the different load stages i.e., no slip can
occur between the two materials.
No bond, no development length, no anchorage, rebar will
pull loose from concrete
2
Help in transferring force
from steel to concrete and concrete to steel.
3. The stress which is acting on the outer interface of steel to the surrounding concrete
is called bond stress.
• Bond stresses are also drastically affected by the
development of tension cracks in the concrete.
• At a point where a crack occurs, all of the
longitudinal tension will be resisted by the
reinforcing bar.
• At a small distance along the bar at a point away
from the crack, the longitudinal tension will be
resisted by both the bar and the uncracked
concrete.
3
Bond Stress
4. Development
Length
is the length of embedment
necessary to develop the full
tensile strength of the bar,
controlled by either pullout or
splitting
4
6. 6
Development Length in tension
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
7. 7
Development Length
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(2) ψ 𝑒 =Coating factor
=1.5 for epoxy-coated bar with cover < 3𝑑 𝑏 or
clear spacing < 6𝑑 𝑏
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
Development Length in tension
8. 8
Development Length
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(2) ψ 𝑒 =Coating factor
=1.5 for epoxy-coated bar with cover < 3𝑑 𝑏 or
clear spacing < 6𝑑 𝑏
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
(3) ψ 𝑠 =reinforcement size factor
=0.8 for No.6 and smaller bars
=1.0 for No.7 and larger bars
Development Length in tension
9. 9
Development Length
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(2) ψ 𝑒 =Coating factor
=1.5 for epoxy-coated bar with cover < 3𝑑 𝑏 or
clear spacing < 6𝑑 𝑏
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
(3) ψ 𝑠 =reinforcement size factor
=0.8 for No.6 and smaller bars
=1.0 for No.7 and larger bars
(4) λ =lightweight aggregate concrete factor
=1.3 for all-lightweight and
sand-lightweight concrete
=1.0 for normal weight concrete
Development Length in tension
10. 10
Development Length
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(2) ψ 𝑒 =Coating factor
=1.5 for epoxy-coated bar with cover < 3𝑑 𝑏 or
clear spacing < 6𝑑 𝑏
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
(3) ψ 𝑠 =reinforcement size factor
=0.8 for No.6 and smaller bars
=1.0 for No.7 and larger bars
(4) λ =lightweight aggregate concrete factor
=1.3 for all-lightweight and
sand-lightweight concrete
=1.0 for normal weight concrete
(3) 𝑐 𝑏 =spacing or cover dimension
(𝑐 𝑏+𝐾𝑡𝑟)
𝑑 𝑏
≤2.5
Development Length in tension
11. 11
Development Length
Tension Development Length Ldt
𝐿 𝑑 =
3
40
×
𝑓𝑦
𝑓′ 𝑐
×
ψ 𝑡ψ 𝑒ψ 𝑠λ
(𝑐 𝑏 + 𝐾𝑡𝑟)
𝑑 𝑏
× 𝑑 𝑏
(2) ψ 𝑒 =Coating factor
=1.5 for epoxy-coated bar with cover < 3𝑑 𝑏 or
clear spacing < 6𝑑 𝑏
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(1) ψ 𝑡(𝛼)=reinforcement location factor
=1.3 for top horizontal reinforcement bars
(i.e., 12” or more of concrete is cast in a
single concreting below the development
length of splice in question)
=1.0 for other reinforcement bars
(3) ψ 𝑠 =reinforcement size factor
=0.8 for No.6 and smaller bars
=1.0 for No.7 and larger bars
(4) λ =lightweight aggregate concrete factor
=1.3 for all-lightweight and
sand-lightweight concrete
=1.0 for normal weight concrete
(3) 𝑐 𝑏 =spacing or cover dimension
(𝑐 𝑏+𝐾𝑡𝑟)
𝑑 𝑏
≤2.5
(3) 𝑓′ 𝑐 ≤ 100psi
Development Length in tension
13. 13
Development Length
Ldt
For No.6 (20mm) and smaller bars, 𝐿 𝑑 =
𝑓𝑦 𝛼
25 𝑓′ 𝑐
× 𝑑 𝑏 ≥ 12"
𝐿 𝑑 =
𝑓𝑦 𝛼
20 𝑓′ 𝑐
× 𝑑 𝑏 ≥ 12"
Simplified Tension Development Length
Modification factor
𝑙 𝑑 may also be modified by (
As required
As provided
)
𝑙 𝑑 ≥12” (in all cases)
For No.7 (22mm) and larger bars,
Development Length in tension
14. 14
Development Length
Ldt
Simplified Tension Development Length
by table
Modification factor
𝑙 𝑑 may also be modified by (
As required
As provided
)
𝑙 𝑑 ≥12” (in all cases)
Development Length in tension
15. 15
Standard Bar Hooks
When desired tensile stress in a bar cannot be developed by bond alone, it is
necessary to provide special anchorage at the end of the bar
Bar Size, db Minimum Diameter, Ø
No.3 (10mm) through No.8 (25mm) 6 𝑑 𝑏
No.9,10 and 11 (No.29,32 and 36 ) 8 𝑑 𝑏
No.14 (43mm) through No.18 (57mm) 10 𝑑 𝑏
Hooked-Bar details for Development of standard hook
(b) Stirrups and Ties
(a) Main Reinforcement
22
16. 16
Development Length of Hooked deformed Bar in
tension, 𝐼 𝑑ℎ
𝐿 𝑑ℎ =
0.02ψ 𝑒λ𝑓𝑦
𝑓′ 𝑐
× 𝑑 𝑏
(1) ψ 𝑒 =Coating factor
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
17. 17
𝐿 𝑑ℎ =
0.02ψ 𝑒λ𝑓𝑦
𝑓′ 𝑐
× 𝑑 𝑏
(1) ψ 𝑒 =Coating factor
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(2) λ =lightweight aggregate concrete factor
=1.3 for all-lightweight and
sand-lightweight concrete
=1.0 for normal weight concrete
Development Length of Hooked deformed Bar in
tension, 𝐼 𝑑ℎ
18. 18
Development Length of Hooked deformed Bar, 𝐼 𝑑ℎ
𝐿 𝑑ℎ =
0.02ψ 𝑒λ𝑓𝑦
𝑓′ 𝑐
× 𝑑 𝑏
(1) ψ 𝑒 =Coating factor
=1.2 for all other epoxy-coated bar
=1.0 for Uncoated and zinc-coated reinforcement
(2) λ =lightweight aggregate concrete factor
=1.3 for all-lightweight and
sand-lightweight concrete
=1.0 for normal weight concrete
For Normal Concrete,
𝐿 𝑑ℎ =
0.02𝑓𝑦
𝑓′ 𝑐
× 𝑑 𝑏
Modification factors
𝑙 𝑑ℎ may be modified by (
As required
As provided
)
For No.11 and smaller bar hooks with side cover ≥2.5” and for 90° hooks
with clear cover on bar extension ≥2.0”, 𝑙 𝑑ℎ is multiplied by 0.7
For No.11 and smaller bars hooks that are enclosed within ties or stirrups
at spacing ≤ 3𝑑 𝑏 along 𝑙 𝑑ℎ, 𝑙 𝑑ℎ is multiplied by 0.8
Development Length of Hooked deformed Bar in
tension, 𝐼 𝑑ℎ
20. 20
Development Length or Anchorage
( 𝑙 𝑑 or 𝑙 𝑑ℎ )
(a) (b) (c)
Hook development length, 𝑙 𝑑ℎ is used only when development length, 𝑙 𝑑 is not adequate
21. 21
Development Length
Compression Development Length Ldc
𝐿 𝑑 =
0.02𝑓𝑦
𝑓′ 𝑐
× 𝑑 𝑏 ≥ 0.0003𝑓𝑦 ≥ 8"
𝐿 𝑑𝑐 shorter than 𝐿 𝑑𝑡
Modification factor
𝑙 𝑑 may be modified by (
As required
As provided
)
For No.4 ties < 4” c/c spacing , 𝑙 𝑑 may also be modified by 0.75
𝑙 𝑑 ≥8” (in all cases)
Hooks shall not be used to develop bars in compression (12.5.5 ACI 318-05)
Development Length in compression
26. Development Length from column to footing
For the case where all the column bars
are in compression, the dowels must
extend into the footing a compression
development length ldc .
(a)Longitudinal bars in column are in
compression
The dowel bars are usually hooked and extend to the level
of the flexural reinforcement in the footing. According to
Section 12.5.5 ACI 318-05, the hooked portion of the
dowels cannot be considered effective for developing the
dowel bars in compression.
26
27. Development Length from column to footing
Either direct or uplift forces or transfer
by a moment tensile force can act from
column, the dowels must extend into
the footing a tension development
length ldt .
(b)Longitudinal bars in column are in
tension
Tensile anchorage of the dowel bars into a footing is
typically accomplished by providing 90-degree standard
hooks at the ends of the dowel bars with the development
length of the hooked bar, ldh, determined in accordance
with Section 12.5 of ACI 318-14.
27
29. Development Length (Lap splice inTension)
29
Class A Splice: 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑡𝑒𝑛……………………….……….……….…..1.0𝑙 𝑑 ≥ 12”
Class B Splice: 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑡𝑒𝑛………………………….….………….…..1.3𝑙 𝑑 ≥ 12”
For No.6 (20mm)
and smaller bars,
𝐿 𝑑 =
𝑓𝑦 𝛼
25 𝑓′ 𝑐
× 𝑑 𝑏
𝐿 𝑑 =
𝑓𝑦 𝛼
20 𝑓′ 𝑐
× 𝑑 𝑏
For No.7 (22mm)
and larger bars,
Lap splicing of No.14 and No.18 bars
in tension is prohibited.
50%
30. Development Length (Lap splice in Compression)
30
𝒇 𝒚 ≤ 60,000 psi 𝒇 𝒚 >60,000 psi
𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑐𝑜𝑚 0.0005𝑓𝑦 𝑑 𝑏 (0.0009𝑓𝑦-24) 𝑑 𝑏 ≥ 12”
For 𝑓′ 𝑐 < 3000 psi, 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑐𝑜𝑚 shell be increased by one-third
Where ties throughout the lap splice length have an effective area ≥ 0.0015h s, lap splice length shall be
permitted to be multiplied by 0.83 ≥ 12”
Lap splicing of No.14 and No.18 bars to No.11 and smaller bars in
compression shell be permitted when
𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑐𝑜𝑚 = larger of [ 𝑙 𝑑𝑐 of larger bar and 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑐𝑜𝑚 of smaller bar ]
31. Development Length (Lap splice in Column)
31
Column – no restrictions Column – no restrictions Column – mid
33. Development Length (Lap splice inTension only in Column)
33
Class A Splice: 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑡𝑒𝑛……………………….……….……….…..1.0𝑙 𝑑 ≥ 12”
Class B Splice: 𝑙 𝑠𝑝𝑙𝑖𝑐𝑒,𝑡𝑒𝑛………………………….….………….…..1.3𝑙 𝑑 ≥ 12”
For No.6 (20mm)
and smaller bars,
𝐿 𝑑 =
𝑓𝑦 𝛼
25 𝑓′ 𝑐
× 𝑑 𝑏
𝐿 𝑑 =
𝑓𝑦 𝛼
20 𝑓′ 𝑐
× 𝑑 𝑏
For No.7 (22mm)
and larger bars,
Lap splicing of No.14 and No.18 bars
in tension is prohibited.
100%
59. Development Length (Lap splice in Beam)
59
Ordinary Moment-Resisting Frame
Beam
Top Bar – Mid
Bot Bar – At Support or 2h
Beam
Top Bar – Mid
Bot Bar – Outside 2h within L/3
60. Development Length (Lap splice in Beam)
60
Ordinary Moment-Resisting Frame
For closed stirrups for torsion spacing, smax =
𝑃ℎ
8
or 12”
61. Development Length (Lap splice in Beam)
61
Intermediate Moment-Resisting Frame Special Moment-Resisting Frame
Outside 2h
ACI 318-05 ACI 318-08
Stirrups
without seismic
hook
Stirrups with
seismic hook
Beam
Top Bar – Mid
Bot Bar – Mid
62. Development Length (Lap splice in Beam)
62
Hoop reinforcement for beams
Crosstie — A continuous reinforcing
bar having a seismic hook at one end
and a hook not less than 90° with at
least a 6db extension at the other
end.
Hoop — A closed tie or continuously
wound tie. A closed tie can be made up
of several reinforcement elements each
having seismic hooks at both ends. A
continuously wound tie shall have a
seismic hook at both ends.
64. Development Length
64
Bars must extend the longer of d or 12db past the flexural cutoff
points except at supports or the ends of cantilevers
Structural Integrity Requirement
65. 65
Simple Supports: At least one-third of the positive moment
reinforcement must be extended 15 cm. into the supports
Structural Integrity Requirement
Development Length
66. 66
Continuous interior beams with closed stirrups: At least one-fourth of the positive moment
reinforcement must be extended 15 cm. into the support
Structural Integrity Requirement
Development Length
67. 67
Continuous interior beams without closed stirrups: At least one-fourth of the positive
moment reinforcement must be continuous or shall be spliced near the support with a
class B tension splice and at non-continuous supports be terminated with a standard hook
Splice Class
ACI 318-05 ACI 318-08
Class A Class B
Structural Integrity Requirement
Development Length
68. 68
Beams forming part of a frame that is the primary lateral load resisting system for the
building.: This reinforcement must be anchored to develop the specified yield strength, fy ,
at the face of the support
Structural Integrity Requirement
Development Length
69. 69
Interior beams: At least one-third of the negative moment reinforcement must be
extended by the greatest of d, 12 db or
𝑙 𝑛
16
past the negative moment point of inflection.
Structural Integrity Requirement
Development Length
70. 70
Perimeter beams: In addition,
1
6
of the (-) reinforcement required at the support must be
made continuous at mid-span. This can be achieved by means of a class B tension splice at
mid-span
Splice Class
ACI 318-05 ACI 318-08
Class A Class B
Structural Integrity Requirement
Development Length
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
During the placing and vibration of the concrete, some air and excess water tend to rise toward the top of the concrete, and some portion may be caught under the higher bars. In addition, there may be some
settlement of the concrete below. As a result, the reinforcement does not bond as well to
the concrete underneath, and increased development lengths will be needed
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
Sir Aung Myat Thu
Pin – No moment – Compression Ldc
Fix base – Moment transfer - Ldt
(c+ktr)/db = 1.5
In high seismic cases cant use modification factor
In high seismic cases cant use modification factor
In high seismic cases cant use modification factor
In high seismic cases cant use modification factor
In high seismic cases cant use modification factor
In high seismic cases cant use modification factor
Cover < 2.5”, 0.8x doesnt not apply
No.4 - 0.5”
In the case of bars in compression, a part of total force is transferred by bond along the embedded length and a part is transferred by end bearing of the bars on the concrete. Because the surrounding concrete is relatively free of cracks and because of the beneficial effect of end bearing, Idc shorter Idt ,
Cover beam , column = 1.5”
Reduce beam size – reduce ld
To develop fy at the face of support
Straight Dowel bar – push straight dowels down into the concrete while it is still in concrete plastic stage.
Theoretically, if the steel column is subjected to axial force only, then yes, there is no need for dowel bars | anchor bolts. But that is rarely the case.
Column bases are almost always subjected to bending moments in addition to compression, sometimes even torsion. Moments and | or torsion causes tension at one side of the column base making it move outwards and upwards.
Development length မလံုေလာက္ခဲ့ရင္ standard 90° hook သံုးၿပီး Ldh ေျပာင္းတြက္ရပါမယ္၊ ဇကာ သံလံုးကို 16mm ကေန 25mm ၾကား သံုးေလ့ ရွိၾကတာမို႔ အၾကမ္းဖ်င္း ေျပာရရင္ေတာ့ 5 ေပ ပတ္လည္ေအာက္ footing ေတြဟာ Ld မလံုေလာက္တတ္ပါဘူး၊ hook လိုအပ္ေလ့ ရွိၾကပါတယ္။
Compression forces are transferred through direct bearing while tension forces are transferred through developed reinforcement. When column sizes are not same, Bot large, top small. Pe.. Eccentricity
The only way the moment can be transfered into the footing is through tension reinforcement that will keep the column from cracking and breaking free from the footing due to the bending moment. T
bar forces are so large they can split the concrete and destroy the effectiveness of the lap splice.
The development length ld used to obtain lap length should be based on fy because the splice classifications already reflect any excess reinforcement at the splice location; therefore, the factor from 12.2.5 for excess As should not be used.
သံေခ်ာင္းတစ္ေခ်ာင္း၏ေပရွည္သည္ 12Meter…39.5Ft ရွိပါသည္။
Tie area >= 0.0015hs
There are no restrictions on the location of lap splices in intermediate or ordinary moment frames.
smax
Note that the column splice should satisfy requirements for all load combinations for the column. Frequently, the basic gravity load combination will govern the design of the column itself, but a load combination including wind or seismic loads may induce greater tension in some column bars, and the column splice should be designed for this tension.
(Reinforcing bars in columns may be subjected to comp or tension or different load combination, both ten and compression. ACI code 12.17 require that a minimum tension capacity be provided in each face of all columns even where analysis indicates compression only. Ordinary compressive lap splices provide sufficient tensile resistance, but end-bearing splices may require additional bars for tension, unless the splices are staggered. )
If bar stress due to factored load is compression, compression splice
When stress is tension <0.5fy, spliced ½ of bar, Class B.
Spliced <=1/2 of bar and splices are staggered by ld, Class A.
When stress is tension >0.5fy, Class B
Max slope 1:6
Can lap 100% in SMRF, according to CQHP 50%
If bar stress due to factored load is compression, compression splice
When stress is tension <0.5fy, spliced ½ of bar, Class B.
Spliced <=1/2 of bar and splices are staggered by ld, Class A.
When stress is tension >0.5fy, Class B
There are no restrictions on the location of lap splices in intermediate or ordinary moment frames.
Note that the column splice should satisfy requirements for all load combinations for the column. Frequently, the basic gravity load combination will govern the design of the column itself, but a load combination including wind or seismic loads may induce greater tension in some column bars, and the column splice should be designed for this tension.
(Reinforcing bars in columns may be subjected to comp or tension or different load combination, both ten and compression. ACI code 12.17 require that a minimum tension capacity be provided in each face of all columns even where analysis indicates compression only. Ordinary compressive lap splices provide sufficient tensile resistance, but end-bearing splices may require additional bars for tension, unless the splices are staggered. )
If bar stress due to factored load is compression, compression splice
When stress is tension <0.5fy, spliced ½ of bar, Class B.
Spliced <=1/2 of bar and splices are staggered by ld, Class A.
When stress is tension >0.5fy, Class B
Max slope 1:6
Support ကေန L/3 အတြင္းမွာ cutting length ျဖတ္ေပးရပါမယ္။ End support / middle support သေဘာတရားအတူတူပါပဲ။ ဘာလို႔လဲဆိုေတာ့ က်ေနာ္တို႔က L/3 ေနရာကို negative moment ကေန positive moment ေျပာင္းတဲ့ေနရာလို႔ ယူဆထားပါတယ္။
Engineering အေခၚအရ point of inflection လို႔ေခၚပါတယ္။ moment zero ျဖစ္တဲ့ေနရာပါ။ တကယ္တမ္းက L/3 ေနရာမွာ point of inflection ျဖစ္ခ်င္မွျဖစ္ပါမယ္။ ကိုယ္တိုင္ moment diagram ဆြဲၾကည့္မွ သိနိုင္ပါမယ္။ ဒါေပမဲ့ L/3 ေနရာဟာ rebar ကို cutting length လုပ္ရင္ safe ျဖစ္တဲ့အတြက္ L/3 ေနရာကိုပဲ လုပ္ငန္းခြင္မွာ ျဖတ္ၾကပါတယ္။
အျခဳပ္ေျပာရရင္ = L/3 ေနရာဟာ negative moment အတြက္ rebar လိုအပ္ခ်က္ လံုေလာက္တယ္လို႔ ယူဆတဲ့အတြက္ L/3 ေနရာမွာ ျဖတ္ျခင္းျဖစ္ပါတယ္။
At locations where analysis indicates flexural yielding caused by inelastic lateral displacements of the frame
ØVc = Ø 2 √f’c bd
Ph = perimeter of stirrup centre
U nyi hla nge – inter – seismic
Lap splices are not to be used:
• Within joints.
• Within 2h
• At locations where analysis indicates flexural yielding
caused by inelastic lateral displacements of the frame.
Column hoops should be configured with at least 3 hoop or crosstie legs restraining longitudinal bars along each face.
A single perimeter hoop without crossties, legally permitted by ACI 318 for small column cross section
Support ကေန L/3 အတြင္းမွာ cutting length ျဖတ္ေပးရပါမယ္။ End support / middle support သေဘာတရားအတူတူပါပဲ။ ဘာလို႔လဲဆိုေတာ့ က်ေနာ္တို႔က L/3 ေနရာကို negative moment ကေန positive moment ေျပာင္းတဲ့ေနရာလို႔ ယူဆထားပါတယ္။
Engineering အေခၚအရ point of inflection လို႔ေခၚပါတယ္။ moment zero ျဖစ္တဲ့ေနရာပါ။ တကယ္တမ္းက L/3 ေနရာမွာ point of inflection ျဖစ္ခ်င္မွျဖစ္ပါမယ္။ ကိုယ္တိုင္ moment diagram ဆြဲၾကည့္မွ သိနိုင္ပါမယ္။ ဒါေပမဲ့ L/3 ေနရာဟာ rebar ကို cutting length လုပ္ရင္ safe ျဖစ္တဲ့အတြက္ L/3 ေနရာကိုပဲ လုပ္ငန္းခြင္မွာ ျဖတ္ၾကပါတယ္။
အျခဳပ္ေျပာရရင္ = L/3 ေနရာဟာ negative moment အတြက္ rebar လိုအပ္ခ်က္ လံုေလာက္တယ္လို႔ ယူဆတဲ့အတြက္ L/3 ေနရာမွာ ျဖတ္ျခင္းျဖစ္ပါတယ္။