Title: Cracking,%20Deflections%20and%20Ductility%20Code%20Provisions%20and%20Recent%20Research
1Cracking, Deflections and DuctilityCode
Provisions and Recent Research
Serviceability and Ductility The Other Limit
States
2Cracking, Deflections and DuctilityCode
Provisions and Recent Research
- Overview
- Code provisions for ductility
- Background to the study
- Codes AS3600, AS5100, EC2, BS5400, BS8110,
CEB-FIP 1990, ACI 318 - Background to prediction of cracking and
deflections - Code provisions for crack widths and stress
limits - Code provisions for deflections
- Recent research
- Conclusions
3Code provisions for ductility
4Background to the study
- Prediction of cracking and deflection
- Why is it important?
- Why is it difficult?
- What do the codes say?
5Prediction of Cracking and DeflectionsWhy is it
important?
- Second order effects
- Load distribution and transfer
- Loads on non-structural members
- Durability
- Code compliance
- Contract conditions
- Client expectations
- Aesthetics
- Clearances, ponding etc.
6Why is it difficult?
- Uncertain or unknown material properties
- Inconsistent and incomplete code provisions
- Inherently random nature of cracking
- Unknown manufacture procedures and construction
programme - Variations in curing procedures and environmental
effects - Complex loading history
7Uncertain or unknown material properties
- Concrete tensile strength creep rupture?
- Concrete stiffness under tension non-linearity?
- Concrete creep and shrinkage properties
- Concrete behaviour under unloading/ reloading
8Inconsistent and incomplete code provisions
- Tensile strength of concrete
- Effect of shrinkage on tensile strength
- Tension stiffening
- Loss of tension stiffening
- Effect of uncracked parts of structure
- Effect of shrinkage
9Unknown manufacture procedures and construction
programme
- Concrete age at loading?
- Time before application of loads or restraints?
- Effect of steam curing
- Locked in thermal stresses?
- Storage, curing
- Differential shrinkage?
10Complex loading history
- Critical sections subject to may be sagging,
hogging, sagging, hogging - Effect of axial load
- Calculation of non-recoverable deflections (eg
creep)
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12What do the codes say?
- Compare AS3600, AS5100, EC2, BS5400, BS8110,
CEB-FIP 1990, ACI 318 - Differing and inconsistent provisions
- No one code covers all significant effects
13Background to prediction of cracking and
deflections
- Formation and propagation of cracks
- Relationship between cracking and section
stiffness - Tension stiffening
- Loss of tension stiffening
- Time related effects
- Creep
- Shrinkage
- Differential shrinkage
- Calculating deflections from section stiffness
14Background to prediction of cracking and
deflections
- Recommended readingConcrete Structures
- Stresses and Deformations
- Ghali Favre and Elbadry
15Formation and propagation of cracks
16Relationship between cracking and section
stiffness
- Tension stiffening
- Displacement of Neutral Axis
- Loss of tension stiffening
17Time related effects
- Creep
- General agreement on mechanism and analysis
approach - Amount and rate of creep variable
- Shrinkage
- Affects both section curvature and effective
cracking stress - No agreed approach to analysis of either effect
- Differential shrinkage
- May have a large effect on section curvature and
deflections - Not specifically covered by any of the codes
studied
18Calculating deflections from section stiffness
- Two approaches in codes
- Effective stiffness approach (ACI and
Australian codes) - Branston equation - Average of cracked and uncracked section
stiffness. - Integrate section curvature along the length of
the member.
19Code provisions for stress limits
- AS 3600, AS 5100 and EC2
- Crack control by stress limits governed by bar
diameter and spacing - AS 5100 has much lower stress limits applicable
to stresses due to permanent loads in exposure
classifications B2, C or U - EC2 limits related to specified crack widths
under quasi-static loading - AS 3600 limits similar to EC2 limits for 0.4 mm
crack width for bar diameter, and 0.3 mm for bar
spacing - AS 5100 limits for exposure classification B2 and
higher similar to EC2 limits for 0.2 mm crack
width - The specified stress limits will result in
substantially higher design crack widths with
increased cover.
20Code provisions for stress limitsStress Limits
for Maximum Bar Diameter
21Code provisions for stress limits Stress Limits
for Maximum Bar Spacing
22Code provisions for stress limits Design crack
widths for maximum stress
23Code provisions for stress limits Design crack
widths for maximum stress
24Code provisions for stress limits Design crack
widths for maximum stress
25Code provisions for crack widths
- AS 3600 and AS 5100
- No requirement for calculation of crack widths
26Code provisions for crack widths
27Code provisions for crack widths -EC2
28Code provisions for crack widths
- EC2 - Notes
- Crack spacing is mainly related to cover depth
- Crack width is directly proportional to crack
spacing - Tension stiffening is limited to 40 of steel
strain without stiffening - Coefficient for long term tension stiffening is
reduced by 1/3 (0.6 to 0.4)
29Code provisions for crack widths
Design surface crack width
BS8110
BS 5400
30Code provisions for crack widths
CEB-FIP 1990 (MC 90) Design crack width
Length over which slip between concrete and steel
occurs
Steel strain at the crack
Steel strain under a force causing stress equal
to concrete tensile strength over concrete
tension area x empirical coefficient
Free shrinkage of concrete (generally negative)
31Code provisions for crack widths
ACI 318 - 89, 99, Gergely-Lutz equation
ACI requirements based on stress limits derived
from the Gergely-Lutz equation
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52Code provisions for deflections
- AS 3600, AS 5100, and ACI 318
53Code provisions for deflections
- AS 3600, AS 5100, and ACI 318 - Notes
- Code provisions based on the Branson Equation
ACI 318 is differently formulated, but gives the
same results. - Ief is the average effective stiffness, applied
over the full length of the member. - Ms is determined at the critical section(s)
specified in the code. - AS 5100 provisions are identical to AS 3600,
(other than a typographical mistake!) - In the Australian codes the cracking moment is
reduced by a factor dependent on the concrete
shrinkage. ACI 318 makes no adjustment to the
cracking moment. - AS 3600 and AS 5100 provide a factor kcs to
account for the effects of creep and shrinkage - kcs 2 - 1.2(Asc / Ast ) gt 0.8
54Code provisions for deflections
- AS 5400 and 8110
- Deflections calculated from integration of
section curvatures - Cracking moment and curvature of cracked sections
allows for a short term concrete tensile stress
of 1 MPa, reducing to 0.55 MPa in the long term. - Shrinkage curvature determined from the free
shrinkage strain, and the first moment of area of
the reinforcement about the cracked or uncracked
section, as appropriate. - BS 5400 tabulates factors based on the
compression and tension reinforcement ratios.
55Code provisions for deflections
- Eurocode 2 and CEB-FIP 1990 (MC 90)
- Members which are expected to crack should behave
in a manner intermediate between the uncracked
and fully cracked conditions and, for members
subjected mainly to flexure, an adequate
prediction of behaviour is given by Expression
(7.18)
56Code provisions for deflections
- Eurocode 2 and CEB-FIP 1990 (MC 90)
57Code provisions for deflections
- Eurocode 2 and CEB-FIP 1990 (MC 90)
- Shrinkage curvatures may be assessed using
Expression (7.21)
58Code provisions for deflections
- Summary
- Australian and American codes based on the
Branson equation, using a uniform average
effective stiffness value. - Australian codes allow for loss of tension
stiffening through a reduction of the cracking
moment related to the free concrete shrinkage. - Allowance for shrinkage curvature in the
Australian codes is simplified and will
underestimate curvature in symmetricaly
reinforced sections. - British codes allow only a low tension value for
cracked sections, which is further reduced for
long term deflections - European codes adopt an intermediate approach for
cracked sections, with an allowance for loss of
tension stiffening. - British and European code provisions for
shrinkage curvature are essentially the same
59Code provisions for deflections
- Summary
- None of the codes included in this study make
specific provision for differential shrinkage for
monolithic construction. - Recent research suggests that loss of tension
stiffening takes place within a few days, and
reduced tension stiffening values should be used
in almost all cases
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64Recent Research
- Beeby, Scott and Jones
- Loss of tension occurs much more quickly than has
previously been assumed, within 20-30 days - Mechanism is cumulative damage, resulting from
loss of tensile strength under load, creep plays
an insignificant part - Evidence that final tension stiffening may be
largely independent of concrete strength.
65Conclusions
- Cracking and deflections may be highly variable,
even under nominally identical conditions - Codes do not make specific provisions for all the
relevant factors - AS 3600 and AS 5100 stress limits may result in
substantially greater crack widths than allowed
in other codes
66Conclusions
- In spite of similar approaches, different code
methods for crack width calculation give highly
variable results. - Eurocode 2 appears to be the most consistent
- Predicted deflections are also highly variable.
- Shrinkage effects are significant, even in
symmetrically reinforced sections. - Allow for loss of tension stiffening
- Consider the possibility of differential
shrinkage