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The Design of Fiber Reinforced Polymers for Structural Strengthening An Overview of ACI 440 Guidelines Sarah Witt Fyfe Company November 7, 2008 1

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Page 1: The Design of Fiber Reinforced Polymers for Structural .... guide for the design and construction of externally bonded frp systems for strengthening concrete structures aci document

The Design of Fiber Reinforced Polymers for Structural

StrengtheningAn Overview of ACI 440

Guidelines

Sarah WittFyfe Company

November 7, 2008

1

Presenter
Presentation Notes
Good Morning – thank you all for getting here early and coming to my presentation of the Design of Fiber Reinforced Polymers, also referred to as FRP or composites, for structural strengthening.
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GUIDE FOR THE DESIGN AND CONSTRUCTION OF EXTERNALLY

BONDED FRP SYSTEMS FOR STRENGTHENING CONCRETE

STRUCTURES

ACI Document 440.2R-08Printed July 2008

Presenter
Presentation Notes
This presentation gives you an overview of the design recommendations provided by the ACI 440.2R document, just republished this past summer. This document improves upon the last version, published in 2002. How many of you have attended other design presentations on the ACI 440.2R document? Great – I’m glad to see people with continued interest in the design of FRP. My presentation will focus on the new parts of the document so as not to repeat too much of what you might already have heard while still touching on some of the most common design issues. So what’s new in the document? The latest version has new sections on Near Surface Mounting FRP, strengthening prestressed member with FRP, and has a lot of improved guidelines for bond and general detailing.
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OutlineStrengthening Concrete Structures

Reasons for strengtheningTypes of FRP strengthening systemsMaterials and properties of FRP strengthening systems

Substrate Preparation/FRP ApplicationRepairProper detailing and installation methodsQuality control

Design PrinciplesStrengthening limitsFlexural strengtheningShear strengtheningAxial strengthening

Reinforcement DetailsBond and delaminationDetailing of laps and splices

Design Examples and Case Studies

Presenter
Presentation Notes
Here is a brief outline of what I will be discussing today. There is a lot of information to cover is an short time so please feel free to stop me and ask questions – I’m trying to condense a lot of information into just a short time. I will be going over why we use FRP for strengthening and then have a brief discussion on surface preparation and quality control. Then I will get into the design process. If we still have some time, I will go over a quick example for flexural strengthening.
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Reasons for Strengthening

Change in useConstruction or design defectsCode changesSeismic retrofitDeterioration

Presenter
Presentation Notes
To start – why would you want to use FRP for strengthening an existing structure? There are many reasons why you as engineers might want to do this. Some of the most common reasons are listed here. Change in use describes an application in which a structure is required to carry additional loads, beyond which it was originally designed. This could be a new planter on a parking deck or office space changing to high density file storage. In an industrial environment, it could describe a situation in which a structure is having additional load applied to it via new equipment. The next category we wish wouldn’t happen, but does on occasion. Poor workmanship or design defects can cause a structure to have inadequate load-bearing capacity. FRP can be used to bring the structure back to the performance level for which it was designed. Code changes or bringing a structure up to a newer, stricter code requires a reevaluation and potential strengthening of the structure. This is another great opportunity to utilize FRP. Seismic Retrofit was one of the very first applications of FRP. Much of the initial research in this area was retrofitting of bridge columns to better perform in a seismic event. Finally we have structural repair to members that have deteriorated due to aggressive environments, general wear and tear of other factors that cause deterioration
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Excessive Loading

Presenter
Presentation Notes
And since a picture speaks a thousand words a few shots of what that might cause you to look to FRP to increase the load carrying capacity of your structure – excessive snow loading.
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Flexural Cracking

Presenter
Presentation Notes
Cracking from shear or flexure
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Overloading

Presenter
Presentation Notes
One of my favorite – over loading in front of the warning sign
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Seismic Loads

Presenter
Presentation Notes
Prevent damage from earthquakes so your structure doesn’t end up looking like this
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Improper Steel Placement

Presenter
Presentation Notes
Improper steel placement or also inadequate steel cover. FRP can used if the rebar ended up right next to the formwork with inadequate cover.
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Impact Damage

Presenter
Presentation Notes
And impact damage – although in a case as bad as this, a new girder will be required…..
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Typical FRP Systems forStrengthening Structures

Wet lay-up systemsUnidirectional fiber sheetsMultidirectional fiber sheetsMechanically applied fiber tows

Prepreg systemsUnidirectional fiber sheetsMultidirectional fiber sheetsMechanically applied fiber tows

Precured systemsUnidirectional laminatesMultidirectional gridsShell elements

Other forms not covered

Section 3.2, Guide:

Presenter
Presentation Notes
So now you have determined that your structure needs help, how can FRP provide a solution? Fiber Reinforced Polymers, referred to as FRP, are a combination of high strength fibers in a polymer matrix. This composite material is applied to a structural member to add additional tension capacity. The two most common methods to install FRP are the wet lay up system and precured systems.
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Typical FRP Systems forStrengthening Structures

Presenter
Presentation Notes
The wet lay up system uses rolls of dry fiber that are saturated with epoxy at the job site. The fibers may be saturated with the use of a machine or by hand. Then the material cures in place on the structural member.
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Typical FRP Systems forStrengthening Structures

Presenter
Presentation Notes
In precured systems, the fibers are saturated with epoxy and cured in the manufacturing plant. They are then shipped to the job site and adhesively bonded to the structural member. The most common types are precured strips and reinforcing bars.
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Typical Fiber Properties

Carbon

Aramid

E-Glass

Presenter
Presentation Notes
With either the wet lay up or precured system, there are three common types of fiber – carbon , glass and aramid. Aramid is the generic term for Kevlar, which is a trademarked name. You can see their comparative properties in this chart. With any of the fiber types, the material behavior is linearly-elastic. These materials exhibit no yielding or strain softening. This important aspect must be closely considered when using these materials for reinforcing and strengthening concrete to avoid a brittle failure. The design portion of this presentation will look at this issue in more detail.
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Substrate Preparation / RepairBond vs. Contact Critical

Contact CriticalRequires intimate contact between the FRP System and the concrete

Confinement of columns

Bond CriticalRequires an adhesive bond between the FRP system and the concrete

Beam, slab and wall strengthening

15

Presenter
Presentation Notes
The first step in any FRP installation is to properly prepare the substrate – that is the surface of the member you want to strengthen. There are two types of applications for FRP that require two different levels of surface preparation. Contact critical applications require only intimate contact between the FRP System and the concrete. For this type of application, you generally need clean, sound, dry concrete. In some cases, paint can even be left on the member. The most classic application that is contact critical is the wrapping of columns. Bond critical applications require an adhesive bond between the FRP and the concrete. The surface preparation for this type of application is more involved. Beam, slab and wall applications are all bond critical.
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Substrate Preparation / Repair

Removal / replacement of unsound concrete

Substrate issues:ACI 503ICRI 03730

200 psi (1.4 MPa) minimum tensile strength2500 psi minimum compressive strength of concrete

Section 6.4, Guide:

Presenter
Presentation Notes
For these applications it is recommended that the tensile strength of the substrate be a minimum of 200-psi in order to sustain the bond stresses that will be induced by the FRP and the concrete needs a minimum compressive strength of 2500 psi. All unsound concrete needs to be removed and replaced.
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Substrate Preparation

Preparation of concrete surface

Section 6.4, Guide:

Minimum ICRI CSP 3

Presenter
Presentation Notes
The concrete surface is mechanically abraded to achieve an ICRI concrete surface profile of 3. More information on the CSP 3 profile can be found in ICRI Publication No. 03732.
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Epoxy Injection

Cracks wider than 0.010 in (0.3 mm) should be injected prior to application of the FRP system.

ACI 224.1

Smaller cracks in aggressive environments may require sealing

Section 6.4, Guide:

Presenter
Presentation Notes
…and finally cracks wider than 0.01 inch need to be injected
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Quality Control & Assurance

Bond testingACI 503RASTM D4541Tension adhesion strengths should exceed 200 psi (1.4 MPa), exhibit failure of the concrete substrate.

Cured thicknessExtract small core samples less than 0.5 in (13 mm) diameterAvoid sampling in high stress areas if possibleRepair using overlapping sheets on filled core.

During-construction:

Presenter
Presentation Notes
As with any construction project, it is important to ensure good quality control. In-field bond testing can be used on bond critical applications to ensure the minimum 200 psi bond strength. On all applications, core sampling can be used to ensure the proper number of layers have been installed.
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Quality Control & Assurance

General Acceptance Criteria for DelaminationsWet Layup

Delaminations less than 2 in2 (1300 mm2) each are permissible:No more than 10 delaminations per 10 ft2 of laminate areaTotal delamination area less than 5% of total laminate area

Delaminations less than 25 in2 (16,000 mm2) may be repaired by resin injection or ply replacement, depending upon the size, number and location of delaminations.Delaminations greater than 25 in2 (16,000 mm2) should be repaired by selectively cutting away the affected sheet and applying an overlapping sheet patch of equivalent plies.

Precured systemsEach delamination must be inspected and repaired in accordance with the engineer’s direction

Post-construction:

Presenter
Presentation Notes
After installation, the whole system should be inspected for material delaminations. Delaminations, or bubbles, are the most common problem with FRP installation. The ACI 440 document provides guidelines on allowable delamination size and proper repair.
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Design Guidelines

Presenter
Presentation Notes
Now on to the design of FRP
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FRP Strengthening Applications

Flexural StrengtheningBeams, Slabs, Walls, etc.

Shear StrengtheningBeams, Columns, Walls, etc.

Axial EnhancementColumn Wrapping, Pressure Vessels

Presenter
Presentation Notes
FRP materials can be used to provide additional flexural strength, shear strength and axial enhancement to existing structural members.
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Strengthening Limits

Limited by strength of other structural componentsColumns, footings, etc.

Limited by other failure mechanismsPunching shear

Loss of FRP should not result in immediate collapse

( ) ( )newLLDLexistingn SSR 75.01.1 +≥φ (9-1)

Section 9.2, Guide:

Presenter
Presentation Notes
In any design situation, there is a limit to how much additional strength may be added. ACI 440.2R provides guidelines on theses limits to ensure that another, less desirable failure is not induced, and to ensure that loss of the FRP will not result in immediate collapse of the structure. This equation was updated in the latest version.
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Structural Fire Endurance

Glass Transition Temperatures of most FRP systems is typically in the range of 140 - 180oF (60 - 80oC)Use of an insulation system can improve the overall fire rating of the strengthened reinforced concrete memberInsulation system can delay strength degradation of concrete and steel, increasing the fire rating of the memberThe contribution of the FRP system can be considered if it is demonstrated that the FRP temperature remains below a critical temperature

Presenter
Presentation Notes
Another strengthening limit on the use of FRP is fire. The polymer resins used in FRP have glass transition temperatures in the range of 140 – 180 degrees Fahrenheit. At these temperatures, the epoxies begin to soften and you can no longer count on the full design strength. However, there has been research in this area and the new ACI document reflects changes in the philosophy based on this additional information. This includes the recognition that the use of an insulation system can improve the overall fire rating of a strengthened reinforced concrete member. Also, the contribution of the FRP system can be considered during the fire event if it can be demonstrated that the FRP temperature will remain below a critical temperature during the fire. The critical temperature is defined as the temperature at which significant deterioration of the FRP properties has occurred.
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Rational Fire Endurance Check

Given cover and fire endurance requirementFind the temperature of the steel & concreteFind a reduced steel & concrete material strengthFind the associated reduced section strengthReduced strength > Unfactored demandNo phi factors or load factors

ACI 216R:

Presenter
Presentation Notes
The general fire philosophy comes from the ACI 216 document, that analyzes the behavior of a structure during a fire. Many of you have probably already used this document for a non FRP project. There are no phi or load factors, and reduced concrete and steel strengths are determined based on degradation in a fire. These values are used to compute a design strength of the member during a fire.
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Rational Fire Endurance Check

From ACI 216R - Reduce material strengths at elevated temperature:

( ) ( )LLDLexistingn SSR +≥

Steel: θyy ff →

Concrete: θcc ff '' →

FRP: *0→fuf

Section 9.2.1, Guide:

(9-2)

Presenter
Presentation Notes
This same philosophy is applied to the analysis of an FRP strengthened structure. The steel and concrete are given appropriately reduced properties and the FRP is discounted. The remaining design strength of the member must satisfy equation 9.2 as shown. However, as mentioned before, the use of coatings will allow higher properties to be used for the concrete and steel. Or the use of coatings and/or special epoxies with higher glass transition temperatures can allow the strength of the FRP to be included, if the temperature of the FRP remains below a critical temperature.
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Maximum Service Temperature

Typical glass transition temperature (Tg) for epoxy 140 -

180oF (60 - 80oC)

Above Tg mechanical properties start to degrade

Service temperature should not exceed Tg - 27°F (Tg – 15°C)

Section 1.3.3, Guide:

Presenter
Presentation Notes
Not to be confused with fire design, the service temperature, that is the ambient temperature that the structural members will see, must be limited to the glass transition temperature minus 27 degrees Fahrenheit.
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Flexural StrengtheningChapter 10, Guide

Typical flexural strength increases up to 40%This limit is based on the Guide’s requirements

Positive and negative moment strengtheningAdd strength to RC and PC membersReduce crack widthsSeismic loadings not covered

un MM >φ (10-1)

Presenter
Presentation Notes
FRP is commonly used for both positive and negative moment strengthening. The goal is to have the design flexural strength be greater than the factored moment.
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Assumptions

Design calculations are based on actual dimensions and material properties.Plane sections remain plane (including FRP).Maximum compressive strainTensile strength of concrete is ignored.FRP has linear-elastic relation to failure.Perfect bond between FRP and concrete (no slip).The shear deformation within the adhesive layer is neglected.

003.0=cuε

Section 10.2.1, Guide:

Presenter
Presentation Notes
The design assumptions used for calculating the flexural strength are very straight forward. They include the assumptions from reinforced concrete analysis along with a few particular to FRP such as: the FRP has a linear elastic relation to failure, there is a perfect bond between the concrete and FRP and the shear deformation within the adhesive layer is neglected.
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Verification of Shear Capacity

Section shear capacity must be sufficient to handle shear forces associated with increased flexural capacity.

Section 10.2.1, Guide:

Presenter
Presentation Notes
The designer must also ensure that the section should have adequate shear strength to handle the increased flexural capacity. Meaning that the increase in flexural capacity should not induce the shear failure.
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Failure Modes

1. crushing of concrete prior to steel yield2. yield of steel followed by concrete crushing3. yield of steel followed by FRP failure4. shear / tension delamination in concrete cover5. FRP debonding from substrate

The desired mode of failure is usually mode 2 or 3.

Section 10.1.1, Guide:

Presenter
Presentation Notes
In addition to the failure modes associated with reinforced concrete, the addition of FRP adds two more failure modes – shear/tension delamination in the concrete cover and FRP debonding. The desired failure mode, even after addition of FRP, is to have the steel yield – since this is the ductile failure mode. Following steel yielding, the concrete can crush or the FRP can fail.
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Effective Strain in FRP

0

100

200

300

400

500

600

0 0.005 0.01 0.015 0.02Strain (in/in)

Stre

ss (k

si)

Effective Strain

Rupture Strain

Presenter
Presentation Notes
As mentioned earlier, fiber reinforced polymer materials are linear elastic to failure. To ensure a margin of safety in the design, the full ultimate strength of the FRP will rarely be realized. The concept of “effective strain” is introduced in the ACI 440.2R guideline. The “effective strain” is the strain level achieved in the FRP when the section fails (due to concrete crushing, FRP debonding, etc.). Note that since FRP materials are 100% linearly elastic, the effective strain is linearly proportional to the stress developed in the FRP material as well.
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Limitation on Strain in FRP

fuff

cfd tnE

f εε 9.0083.0'

≤= (10-2) US

To prevent debonding in regions away from FRP Termination

(10-2) SI

fdbicufe cch εεεε ≤−⎟⎠⎞

⎜⎝⎛ −

= (10-3)

fuff

cfd tnE

f εε 9.041.0'

≤=

Presenter
Presentation Notes
In the latest document, new limitations have been provided to ensure that the FRP does not debond in regions away from the termination points. I don’t expect you remember these equations, but know that they are there as guidelines.
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Calculation Procedure

Estimated c = c for Equilibrium?

Estimate neutral axis, c

Determine initial strain in substrate

Determine failure mode

Calculate material strain

Calculate stresses and forces

Check Equilibrium (Calculate c)

Compute Moment Capacity

Check service conditions

YesNo

Presenter
Presentation Notes
So here is an overview of the calculation procedure for flexural strengthening which is an iterative process– First you determine the initial strain in the substrate. This is important because the strain in the FRP is only the strain caused by loads after the installation of the FRP. Any initial strains in the member prior to FRP installation are not counted in the design strain. Then an estimate is made for the neutral axis. A failure mode is determined, and the FRP design strain is calculated. Then the stresses and forces are calculated based on the assumed neutral axis. Equilibrium is checked which calculates a value for c. If this value is the same as the initial assumption – great. Chances are though that the initial c value needs to be adjusted, and the process reiterated until it matches the final value. This may take a few iterations. Once they match, you can compute the section moment capacity and check services conditions.
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Estimate the Neutral Axis DepthNo closed form solution existsMust find depth to the neutral axis by trial and errorAs a starting point, a good rule of thumb is 20% of the effective section depth

dc 20.0≈

c

εs

εfe εbiεb

εc

Presenter
Presentation Notes
So – to go over that step by step – after first determining the initial strains in the substrate, you estimate a value for c. A good starting point is 0.20d.
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Determine Mode of Failure

Concrete Crushing Controls

FRP Rupture Controls

(10-3)fdbicufe cch εεεε ≤−⎟⎠⎞

⎜⎝⎛ −

=

fdbicufe cch εεεε ≤−⎟⎠⎞

⎜⎝⎛ −

=

fdbicufe cch εεεε ≥−⎟⎠⎞

⎜⎝⎛ −

=

Presenter
Presentation Notes
Then you determine the failure mode. If the design strain, based on the assumed c, is smaller than the rupture strain, debonding of the FRP controls. If the design strain is larger, concrete crushing controls. This is important because….
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Concrete Stress Block

Whitney stress block is valid only when concrete crushing governs failure (i.e., εc=0.003)If FRP rupture controls, a stress block appropriate for the concrete strain level should be used

ActualStress

Distribution

EquivalentStress

Distribution

γf 'c

β1cc

Presenter
Presentation Notes
ACI 318 uses the Whitney stress block model for estimating the compressive stress distribution. This model is only valid when concrete crushing is governing failure. If FRP failure governs failure, the strain level in the concrete may be substantially lower than 0.003-in/in. The Whitney stress block will not give an equivalent stress distribution for this condition. The actual non-linear stress distribution in the concrete must be considered or an alternative equivalent stress block model must be employed.
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Concrete Stress Block

( ) ( )[ ]( ) ( )22

1

1 1ln tan42

cccc

cccc

εεεεεεεεβ′+′′−′

−=−

( )cc1

2c

2c1900

ε′εβε′ε+

=γ ln.

c

cc E

f711 ′=ε′

.

εc < 0.003

γf'c

β1c

Presenter
Presentation Notes
One equivalent stress block model, for concrete strains less than 0.003-in/in, is shown here. Once again, don’t worry about the whole equation, just know remember the general design process.
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Calculation of Flexural StrainAssume strain compatibilityBased on failure modeCalculate the strain in each material by similar triangles

( ) ⎟⎟⎠

⎞⎜⎜⎝

−−

+=cdcd

fbifes εεε (10-10)

c

εs

εfe εbiεb

εc

Presenter
Presentation Notes
With the strain in the FRP determined, the strain level in the steel reinforcement and concrete can be determined.
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Calculation Of Stress

ysss fEf ≤= ε

Steel – Elastic / Plastic:

fesfe Ef ε=FRP – Elastic:

(10-11)

(10-9)

StrainSt

ress FRP

Steel

Presenter
Presentation Notes
With the strain level in each material, the stresses in each material can be determined as well. For the steel reinforcement (which is idealized as elastic-perfectly plastic), Eqn 10-9 will indicate the stress level in the steel. For the FRP (which is idealized as perfectly elastic), the stress level can be determined from Eqn 10-9.
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Check Force EquilibriumSum forces in the horizontal directionIf forces do not equilibrate, revise “c”Repeat previous steps

bffAfA

cc

fefssest ′

+=

11αβ Asfs

α1f'cβ1c

Afff

Presenter
Presentation Notes
With all of the material stresses determined, internal force equilibrium may be checked. If the neutral axis depth, c, determined by the equation shown is different from the estimated neutral axis depth, then force equilibrium is not satisfied. The neutral axis depth must then be revised and the iterative process repeated until force equilibrium is satisfied. You can see that this analysis is the same as used for reinforced concrete, with the addition of the FRP force at the bottom of the section.
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Ultimate Strength Model

εfe εbiAf = n tf wfffe = Ef εfe

fsεs

εc

c

⎟⎠⎞

⎜⎝⎛ −+⎟

⎠⎞

⎜⎝⎛ −=

2211 chfAcdfAM feffssnβψβ

(10-13)

Presenter
Presentation Notes
With strain compatibility and force equilibrium satisfied, the nominal moment strength of the reinforced/strengthened concrete section may be determined.
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Loss in Ductility

( )

⎪⎪⎩

⎪⎪⎨

<<−

−+

=

syt

tsysy

syt

t

for

for

for

εε

εεεεε

ε

φ

65.0

005.0005.0

25.065.0

005.090.0

ACI 318 :A section with lower ductility should compensate with a higher reserve of strength

(10-5)

0.90

0.65

φ

Steel Strain at Ultimate

εsy 0.005

ρb

≈0.75ρb

Presenter
Presentation Notes
Following the philosophy of ACI 318, guidelines are given for appropriate phi factors based on section ductility.
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Design Flexural Strength

⎥⎦

⎤⎢⎣

⎡⎟⎠⎞

⎜⎝⎛ −+⎟

⎠⎞

⎜⎝⎛ −=

2211 chfAcdfAM fefssnβψβφφ

Reduction factor for FRP contribution: 85.0=ψ

(10-13)

(10-1)un MM >φ

Presenter
Presentation Notes
With the strength reduction factor, phi, computed based on ductility, the design moment strength may be computed. Please note that there is also a reduction factor for the FRP contribution. This partial reduction factor is used in recognition of the fact that FRP reinforcement is not as statistically reliable as internal steel reinforcement.
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45

ServiceabilityAt service, stress in steel should be limited to 80% of yield strength:

yss ff 80., ≤ (10-6)

Curvature

Mom

ent

Unstrengthened

FRP Strengthened

Ms

My

Mu

Presenter
Presentation Notes
A final check for serviceability should be made to ensure that at service, the stress in the steel is below 80% of the yield strength.
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46

Prestressed Concrete MembersAssumptions

Assumptions for concrete members applystrain compatibility for strain or change in strain in the prestressing steel prestressing steel rupture mode should be investigatedwhere prestressing steel is draped several sections should be evaluated

Presenter
Presentation Notes
This same design philosophy can be extended to prestressed members. A few more assumptions are made in the design process – there is strain compatibility in the prestressing steel and in the case of draped steel, several sections along the length of the member should be checked. Note that the design equations in the latest ACI 440.2R can be applied to bonded prestressed members. The design for unbonded prestressed members is still being evaluated.
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47

Prestressed Concrete MembersFailure Modes

1. Strain level in FRP governed by strain limitations due:1. concrete crushing2. FRP rupture3. FRP debonding4. Prestressing steel failure

Presenter
Presentation Notes
Adding on to the evaluation of failure modes, you must also consider prestressing steel failure
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48

To maintain a sufficient ductility the nominal strain in the prestressing steel should be higher than 0.013. If this strain is not achieved a lower strength factor should be used

Prestressed Concrete MembersStrength Reduction Factor

( )( )

⎪⎪⎩

⎪⎪⎨

<<−

−+

=

010.065.0

013.0010.0010.0013.0010.025.0

65.0

013.090.0

ps

psps

ps

for

for

for

ε

εε

ε

φ (10-19)

Presenter
Presentation Notes
As with non prestressed sections, appropriate phi factors are chosen based on ductility.
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49

In service stress in the prestressing steel should be prevented from yielding:

Prestressed Concrete MembersServiceability

pysps ff 82.0, ≤

pusps ff 74.0, ≤

(10-20a)

(10-20b)

Presenter
Presentation Notes
And serviceability must be checked.
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50

•The calculation procedure for nominal strength:• satisfy should strain compatibility•satisfy force equilibrium•consider mode of failure•similar to method for reinforced members

Prestressed Concrete MembersNominal Strength

Presenter
Presentation Notes
The nominal strength is calculated in a similar method to reinforced sections
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51

For a given value of the neutral axis, c:

Prestressed Concrete MembersNominal Strength

feffe Ef ε=

035.01 2

2

≤+⎟⎟⎠

⎞⎜⎜⎝

⎛++= pnet

cc

epeps r

eEA

P εεε

Stress level in the FRP

Strain in the tendon

(10-21)

(10-22)

Presenter
Presentation Notes
The appropriate stress and strain values are computed
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52

The value of enet depends on the mode of failure

Prestressed Concrete MembersNominal Strength

⎟⎟⎠

⎞⎜⎜⎝

⎛ −≤

ccd p

pnet 003.0εconcrete crushing

FRP rupture or debonding ( ) ⎟

⎟⎠

⎞⎜⎜⎝

−−

+≤cdcd

f

Pbifepnet εεε

(10-23a)

(10-23b)

Presenter
Presentation Notes
Modes of failure are evaluated
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53

Force equilibrium can be checked by satisfying:

Prestressed Concrete MembersNominal Strength

bffAfA

cc

fefpsp

1'

1 βα+

= (10-25)

Presenter
Presentation Notes
And equilibrium is satisfied
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54

Case Study – Slab Upgrade

P/T flat slab live load increase:

50 – 100 psf

Presenter
Presentation Notes
And just to give you a break from looking at slides with equations, a picture of a slab strengthening project using FRP. A change of use in the garage resulted in an increase in the required loading from 50 to 100 psf. FRP was used to add additional moment capacity.
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55

Case Study – Slab Upgrade

Positive moment upgrade to column strip

Presenter
Presentation Notes
Another case of positive moment strengthening.
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56

Shear StrengtheningChapter 11, Guide

un VV >φ

Increase shear capacity of beams or columnsAmount of increase depends on section geometry, existing reinforcement, and a variety of additional factors.

Change failure mode to flexuralTypically results in a more ductile failure

(11-1)

Presenter
Presentation Notes
On to shear strengthening. Similar to flexural strengthening, the nominal shear strength must be greater than the design shear strength.
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Wrapping Schemes

Fully Wrapped “U-wrap” Two sides bonded

Overlap

Presenter
Presentation Notes
The FRP material can be wrapped around the entire cross section, in a “U” wrap configuration, or simply bonded to two sides of the member. Fully wrapped sections are often impractical for beams as it is necessary to penetrate through the adjoining slab or flange. However, this is quite common and practical for shear strengthening of concrete columns.
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Effective Strain in FRP

Maximum strain that can be achieved in the FRP system at the ultimate load stageGoverned by the failure mode of the FRP system and the strengthened member.

memberswrappedcompletelyforfufe εε 75.0004.0 ≤=

pliesfaceorwrapsUbondedforfuvfe −≤= 004.0εκε

(11-6a)

(11-6b)

Presenter
Presentation Notes
And with FRP shear reinforcement, the concept of strain limitations or effective strain is again employed. For completely wrapped members, loss of aggregate typically controls the failure. This is assumed to occur at a strain level of 0.004-in/in. Thus the effective strain in these applications is assumed to be 0.004-in/in. For applications where the material is wrapped on three sides or just bonded on the two faces of the beam, the strain value is a percentage of the ultimate strain, calculated as kv.
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Effective Strain Limitations for FRPDetermination of bond-reduction coefficient κv:

75.0468

Lkk

fu

e21v ≤

ε=κ (11-7) US

75.0900,11

21 ≤=fu

ev

Lkkε

κ

3/2'c

1 4000f

k ⎟⎟⎠

⎞⎜⎜⎝

⎛= (11-9) US

3/2'c

1 27f

k ⎟⎟⎠

⎞⎜⎜⎝

⎛=

⎪⎪⎩

⎪⎪⎨

−−

=bondedsidestwofor

dLd

wrapsUford

Ld

k

f

ef

f

ef

22

(11-7) SI(11-9) SI

(11-10)

Presenter
Presentation Notes
The percentage, kv, is a function of the strength of the concrete and wrapping scheme used. This is evident in the series of equations shown. Note also that the effective strain is limited to 75% of the ultimate elongation to account for the less common FRP rupture failure mode. Kv is a function of factors k1 and k2 and an active bond length Le.
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Effective Strain Limitations for FRPDetermination of active bond length Le:

(11-8) US( ) 58.0ff

e Etn2500L = ( ) 58.0

ffe

Etn300,23L = (11-8) SI

Le

Presenter
Presentation Notes
It has been observed that when FRP bonded to concrete is in direct tension the majority of bond stresses are carried over a relatively small length of the FRP. This length is shown as Le.
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61

Effective Strain Limitations for FRPDetermination of bond-reduction coefficient κv:

75.0468

Lkk

fu

e21v ≤

ε=κ (11-7) US

75.0900,11

21 ≤=fu

ev

Lkkε

κ

3/2'c

1 4000f

k ⎟⎟⎠

⎞⎜⎜⎝

⎛= (11-9) US

3/2'c

1 27f

k ⎟⎟⎠

⎞⎜⎜⎝

⎛=

⎪⎪⎩

⎪⎪⎨

−−

=bondedsidestwofor

dLd

wrapsUford

Ld

k

f

ef

f

ef

22

(11-7) SI(11-9) SI

(11-10)004.0≤= fuvfe εκε

Presenter
Presentation Notes
So going back to the formulas for kv, you insert the correct values for k1, k2 and Le and determine the effective strain
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62

Pertinent Shear Dimensions

df

wf

sf

wf

sf

β

( )f

ffefvf s

dcossinfAV

α+α=

fffv wnt2A =

ffefe Ef ε=

(11-3)

(11-4)

(11-5)

α

Presenter
Presentation Notes
With the effective strain computed, the shear contribution of the FRP reinforcement can be simply calculated by the equations shown, working from the bottom up. Note that these equations are very similar to the equations used to compute the contribution of internal steel stirrups to the shear strength.
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63

Design Shear Capacity

( )ffscn VVVV ψφφ ++=

( )

)(85.0

)(95.0)318(85.0

pliesfaceorwrapsUbonded

wrappedfullyACI

VVVV

f

f

fscn

−=

==

++=

ψ

ψφ

ψφφ

(11-2)

Presenter
Presentation Notes
The overall design shear capacity can be obtained from summing the contribution of the concrete, steel, and FRP as shown in Eqn 11-2 with the appropriate strength reduction factors. Note that the overall strength reduction factor, phi, is the same as for regular steel reinforced concrete and that a reduction factor is again applied to the FRP. This reduction factor on the FRP is 0.85 for bonded applications and 0.95 for fully wrapped applications. This is done in recognition of the fact that fully wrapped applications are more statistically reliable than bonded applications.
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64

Spacing, Reinforcing Limits

4max,dws ff +=

dbfVV wcfs '8≤+

bdf66.0VV cfs ′≤+

(11-11) US

Section 11.1, Guide:

Based on ACI 318-05, Section 11.5.6.9:

(11-11) SI

Presenter
Presentation Notes
A final note on shear strengthening that has been added in the latest ACI version. It is important to maintain reasonable spacing of FRP stirrups just as with steel stirrups. The maximum spacing that will ensure that the FRP reinforcement crosses a potential shear crack is given in the equation shown. There is also an upper limit on the total amount of shear reinforcement that can be provided given by Eqn (11-11). This criteria is similar to the criteria given by ACI 318 to prevent crushing of the compression strut developed in the concrete under shear loads.
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65

Case Study – Precast Garage

Installed FRP “U” Wraps

Presenter
Presentation Notes
And finally another picture of an installed FRP strengthening system for beam shear. This picture shows one of the major advantages of FRP in that you only have to install the material where it is needed. This makes it a very cost effective repair solution.
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66

ConfinementChapter 12, Guide

Increase in member axial compressive strengthEnhance the ductility of members subjected to combined axial and bending forcesIncrease the strength of members subjected to combined axial and bending forces

Presenter
Presentation Notes
In the latest version of ACI, there has been improvements to the section on confinement.
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67

Axial Compression

Fibers oriented transverse to the longitudinal axis of the member

Contribution of any longitudinal fibers to axial strength is negligible

Results in an increase in the apparent strength of the concrete and in the maximum usable compressive strain in the concretePassive confinement

Intimate contact between FRP system and member is critical

Presenter
Presentation Notes
The analysis is based on orienting the fibers transverse to the longitudinal axis of the member. This results in an increase in the apparent strength of the concrete and the maximum usable compressive strain in the concrete. This is an example of a contact critical application, that we discussed earlier.
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Confinement

Confining Pressure

Presenter
Presentation Notes
Confinement of a circular section is well understood. The FRP material, shown in blue, provides a confining pressure around the column.
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69

FRP Confined Concrete Behavior

ccf ′

ccuε

cf ′

Longitudinal StrainTransverse Strain (Dilation)

Stre

ss

Unconfined Concrete

FRP Confined Concrete

εL

εT

Longitudinal Strain

Transverse Strain

cf ′85.0

cε ′ 003.0=cuεfuε feε

Presenter
Presentation Notes
This chart shows the improvement of the behavior of confined concrete
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70

FRP Confined Concrete

Strain Limitation

fufe εκε ε≤= 004.0

Longitudinal StrainTransverse Strain (Dilation)

fufe εκε ε= (12-5)

(12-12)

For pure axial loading:

For combined axial + bending:

55.0=εκ Recommended value (accounts for premature failure strain of FRP)

Limit to maintain shear integrity of concrete

Presenter
Presentation Notes
Designing FRP confined concrete is also, like shear and flexure, based on limiting the design strain. This is to account for premature failure strain of the FRP and to maintain shear integrity of the concrete.
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71

FRP Confinement Model

ccu

ccc ffEε

′−′=2

( )

⎪⎩

⎪⎨⎧

≤≤′+′

′≤≤′

−−=

ccuctcc

tccc

ccc

c

forEf

forfEEEf

εεεε

εεεε

2

22

2 04

2

2EE

f

c

ct −

′=′ε

Longitudinal StrainTransverse Strain (Dilation)

Where,

Stre

ss

Unconfined Concrete

FRP Confined Concrete

Ec

E2

Strain

ccf ′

cf ′

tε ′cε ′ ccuε

(12-2a)

(12-2b)

(12-2c)

Presenter
Presentation Notes
The confinement model used by ACI 440.2R is based on the stress and strain model by Lam and Teng.
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72

FRP Confinement Model

⎟⎟

⎜⎜

⎛⎟⎟⎠

⎞⎜⎜⎝

⎛′′

+′=45.0

1250.1c

fe

c

lbcccu f

fεε

κεε

lafccc fff κψ 3.3+′=′

Longitudinal StrainTransverse Strain (Dilation)

Where,

fl is the confining pressure exerted by the FRP jacket

κa and κb are shape factors

Stre

ss

Unconfined Concrete

FRP Confined Concrete

Ec

E2

Strain

ccf ′

cf ′

tε ′cε ′ ccuε

(12-3)

(12-6)

Presenter
Presentation Notes
Here are the equations used – they include a shape factor Ka and Kb…
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73

Circular Sections

Ef εfe

FRP Jacket

fl

flEf εfe

fl

Concrete0.1== ba κκ

Shape factors:

DtnE

f feffl

ε2= (12-4)

Confining pressure:

Presenter
Presentation Notes
Which are 1 for circular sections.
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74

Rectangular Sections

b

h

D 22 hbD +=

DtnE

f feffl

ε2= (12-4)

Confining pressure:

Equivalent circular column

Presenter
Presentation Notes
The confining pressure equations for rectangular sections are limited to those columns with an aspect ratios of less than 2 and face dimension less than 36 inches. Of course, as with most design cases, if testing can be used to demonstrate the effectiveness for other dimensions, FRP can be used.
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75

Rectangular Sections

2

⎟⎠⎞

⎜⎝⎛=

hb

AA

c

eaκ

b

h

Effective confinement area, Ae

5.0

⎟⎠⎞

⎜⎝⎛=

bh

AA

c

ebκ

Shape factors:

(12-9)

(12-10)

Confining stress concentrated at corners

Presenter
Presentation Notes
This shows the effective confinement area and the equations for the shape factors for rectangular columns.
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76

Rectangular Sections

Ratio of effective confinement area to total area of concrete

( ) ( )

g

gg

cc

c

e A

rbbhrh

hb

AA

ρ

ρ

−⎥⎦

⎤⎢⎣

⎡−⎟

⎠⎞

⎜⎝⎛+−⎟

⎠⎞

⎜⎝⎛

−=

13

221

22

(12-11)

Presenter
Presentation Notes
The ratio of effective confinement area to total area is calculated using this rather large equation. It is interesting to note that is based on corner radius (Rc). The larger the radius of your corners, the more effective the FRP wrap, as the confinement is provided in from the corners.
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77

Using the Confinement Model

( )[ ]stystgccn AfAAfP +−= '85.085.0 φφ

with existing steel spiral reinforcing

with existing steel-tie reinforcing:

( )[ ]stystgccn AfAAfP +−= '85.080.0 φφ

Compressive Strength:

(12-1a)

(12-1b)

Use the confined concrete compressive strength in ACI 318 equations

Presenter
Presentation Notes
The calculated increased compressive strength of the concrete is used in the axial load equations from ACI 318.
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78

Serviceability Considerations-Axial Compression

To ensure radial cracking will not occur under service loads,

'65.0 cc ff ≤

To avoid plastic deformation under sustained or cyclic loads,

ys ff 60.0≤

Section 12.1.3, Guide:

Presenter
Presentation Notes
And serviceability must be checked for axial compression as well.
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79

Reinforcement DetailsChapter 13, Guide

General Guidelines:Do not turn inside corners;Provide a minimum 1/2 in. (13 mm) radius when the sheet is wrapped around outside cornersProvide adequate development length

Provide sufficient overlap when splicing FRP plies.

Presenter
Presentation Notes
So the last section for design is reinforcement details. You all have been great for sticking with me through the technical parts of this presentation. Reinforcement details are very important for FRP design and they have been improved in the latest version of 440.2R. I will highlight these quickly just to give you an idea of what to look for that is unique for FRP. Well, let me start with what is not unique. FRP must have sufficient bond length and properly detailed splices, just like with rebar.
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80

Allowable Termination Points –Simply Supported Beams

Plies should extend a distance equal at least to ldfpast the point along the span corresponding to the cracking moment, Mcr, If Vu > 0.67Vc at the termination point the FRP laminate should be anchored with transverse (“clamping”) reinforcement

Section 13.1.2, Guide

Presenter
Presentation Notes
Successive layers of the material must be staggered at the ends. Each layer should extend 6” past the previous layer.
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81

Bond and DelaminationTransverse (“clamping”) reinfocement

Area of transverse (“clamping”) FRP U-Wrap reinforcement to prevent concrete cover layer from splitting:

( )( )

anchorfuvf

allongitudinfufanchorf E

fAA

εκ= (13-1)

Presenter
Presentation Notes
FRP u-wraps may be used at the ends of the beam to prevent the concrete cover layer from splitting. This detail should be used when the factored shear at the termination point is greater than 2/3 of the concrete shear strength. Basically, its an extra anchor for the flexural strengthening in areas of high shear.
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82

Development Length

The bond capacity of FRP is developed over a critical length:

'057.0

c

ffdf

f

tEnl =

(13-2)

'c

ffdf

f

tEnl =

in in.-lb units

in SI units

Presenter
Presentation Notes
Equations for development length of externally bonded material
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83

Detailing of NSM bars

groove dimensions shall be at least 1.5 times the diameter of the barFor a rectangular bar the minimum groove size shall be 3ab x 1.5bb

Presenter
Presentation Notes
And finally, a few details for NSM. I have not specifically mentioned near surface mounting as the equations I have talked about are all applicable, but to finish I will just mention for those of you who are not familiar with this technology. Near Surface mounting involves taking bars or rods made from FRP and placing them in grooves at the surface of the member. This picture shows a picture of both options. It is important to properly detail the groove dimensions.
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84

Development Length of NSM bars

Development length of NSM bar:

( ) fdb

db fdlmax5.04 τ

=

( )( ) fdbb

bbdb f

badal

max5.02 τ+=

Development length of NSM bar:

for rectangular bars

for circular bars (13-3)

(13-4)

Presenter
Presentation Notes
And calculate the development length. So with that….
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QUESTIONS?

Thank You

85

Presenter
Presentation Notes
I will ask if there are any questions.
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86

Design Example

Flexural Strengthening of Interior Beam

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87

Manufacturer’s reported FRP-system properties

24’-0”

w

DL,wLL

ELEVATION SECTION

12”

21.5”

24”f’c=5000 psi

3-#9 barsfy=60 ksi

FRP

2-12”x 23’-0” FRP pliesφMn=266 k-ft

(w/o FRP)

Thickness per ply, 0.040 in. 1.016 mm

Ultimate tensile strength 90 ksi 0.62 kN/mm2

Rupture strain, 0.015 0.015

Modulus of elasticity of FRP laminates, 5360 ksi 37 kN/mm2

Design Example: Flexural Strengthening of an Interior Beam

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88

Loadings and corresponding moments

Two, 12 in. wide by 23 ft. long plies are to be bonded to the soffit of the beam using the wet-lay-up technique.

Loading/Moment Existing loads Anticipated loadsDead loads, wDL 1.00 k/ft 14 N/mm 1.00 k/ft 14 N/mmLive load, wLL 1.20 k/ft 17 N/mm 1.80 k/ft 26 N/mm

Unfactored loads, (wDL + wLL) 2.20 k/ft 32.1 N/mm 2.80 k/ft 40.9 N/mm

Unstrengthened load limit (1.1wDL +0.75wLL) n/a n/a 2.45 k/ft 34.9 N/mm

Factored loads, (1.2wDL +1.6wLL) 3.12 k/ft 50.2 N/mm 4.46 k/ft 65.1 N/mm

Dead-load moment, MDL 72 k-ft 96.2 kN-m 72 k-ft 96.2 kN-mLive-load moment, MLL 86 k-ft 114.9 kN-m 130 k-ft 173.6 kN-m

Service-load moment, Ms 158 k-ft 211.1 kN-m 202 k-ft 269.8 kN-mUnstrengthened moment limit (1.1MDL +0.75MLL) n/a n/a 177 k-ft 240 kN-m

Factored moment, Mu 224 k-ft 303.6 kN-m 294.4 k-ft- 399.2 kN-m

Design Example: Flexural Strengthening of an Interior Beam

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89

• Step 1 - Compute the FRP-system design material properties

*fuEfu fCf =

*fuEfu C εε =

For an interior beam, an environmental-reduction factor (CE ) of 0.95 is suggested.

85ksiksi)(0.95)(90 ==fuf

in.0.0142in./15in./in.)(0.95)(0.0 ==fuε

Design Example: Flexural Strengthening of an Interior Beam

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90

• Step 2 - Preliminary calculations

Properties of the concrete:

β1 from ACI 318-05, Section 10.2.7.3.

1'1.05 0.05 0.80

1000cfβ = − =

psi4,030,000psi500057,000 ==cE

Design Example: Flexural Strengthening of an Interior Beam

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91

Properties of existing reinforcing steel:

bdAs

s ≡ρ

22 in.3.00)in.3(1.00 ==sA

( )( ) 0.0116in.21.5in.12

in.3.00 2

==ρ s

Design Example: Flexural Strengthening of an Interior Beam

• Step 2 - Preliminary calculations

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92

• Step 2 - Preliminary calculations

Properties of the externally bonded FRP reinforcement:

fff wntA =

bdAf

f ≡ρ

( )( )( ) 2ply

in. 0.96in.in. 120.040plies 2 ==fA

( )( ) 0.00372in. 21.5in. 12

in. 0.96 2

==fρ

Design Example: Flexural Strengthening of an Interior Beam

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93

• Step 3 - Determine the existing state of the strain on the soffit

The existing state of strain is calculated assuming the beam is cracked and the only loads acting on the beam at the time of the FRP installation are dead loads. A cracked section analysis of the existing beam gives k=0.334 and Icr=5937 in.4

ccr

DLbi EI

kdhM )( −=ε

( ) ( )( )[ ]( )( )

0.00061ksi4,030in.5,937

in.21.50.334in.24in.k8644

=

−⋅=

bi

bi

ε

ε

Design Example: Flexural Strengthening of an Interior Beam

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94

0128.0)0142.0(9.00113.0 =≤=fdε

• Step 4 – Determine the design strain of the FRP System

( ) ( ) fufd inpsipsi εε 9.0

04.0000536025000083.0 ≤=

Design Example: Flexural Strengthening of an Interior Beam

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95

• Step 5 - Estimate c, the depth to the neutral axis

A reasonable initial estimate of c is 0.20d. The value of c is adjusted after checking equilibrium.

dc 20.0= ( )( ) in. 4.30in. 21.50.20 ==c

Design Example: Flexural Strengthening of an Interior Beam

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96

• Step 6 - Determine the effective level of strain in the FRP reinforcement

fdbif

fe ccd

εεε ≤−⎟⎟⎠

⎞⎜⎜⎝

⎛ −= 003.0

009.000061.03.4

3.424003.0 ≤−⎟⎠⎞

⎜⎝⎛ −

=feε

009.00131.0 ≤=feε

009.0=feε

Design Example: Flexural Strengthening of an Interior Beam

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97

Since FRP controls the section failure, the concrete strain is less than 0.003:

( ) ⎟⎟⎠

⎞⎜⎜⎝

−+=

cdc

fbiefc εεε

( ) 0021.03.424

3.400061.0009.0 =⎟⎠⎞

⎜⎝⎛

−+=cε

Design Example: Flexural Strengthening of an Interior Beam

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98

• Step 7 - Calculate the strain in the existing reinforcing steel

( ) ⎟⎟⎠

⎞⎜⎜⎝

−−

+=cdcd

fbifes εεε

( ) 0084.030.42430.45.2100061.0009.0 =⎟

⎠⎞

⎜⎝⎛

−−

+=sε

Design Example: Flexural Strengthening of an Interior Beam

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99

• Step 8 - Calculate the stress level in the reinforcing steel and FRP

ysss fEf ≤ε=

feffe Ef ε=

ksi60ksi348ksi60)0084.0)(ksi000,29(s

≤=≤=

sff

( )( ) ksi.2840.009ksi5,360 ==fef

Design Example: Flexural Strengthening of an Interior Beam

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100

• Step 9a - Calculate the internal force resultants

Approximate stress block factors may be calculated using the parabolic stress-strain relationship of concrete as follows:

0021.010030,4

)000,5(7.17.16

'' =

×==

c

cc E

Design Example: Flexural Strengthening of an Interior Beam

749.0)0021.0(2)0021.0(6

0021.0)0021.0(426

4'

'

1 =−−

=−−

=cc

cc

εεεεβ

886.0)0021.0()749.0(3)0021.0()0021.0(3

33

22'

2'

1 ==−

=c

ccc

γεεεεα

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101

• Step 9b – Check equilibrium

Force equilibrium is verified by checking the initial estimate of the neutral axis, c

Design Example: Flexural Strengthening of an Interior Beam

inbcfAAfA

cc

fefss 87.5)12)(749.0)(5)(886.0()2.48)(96.0()60)(3(

1'

1

=+

=+

=βα

NGininc 30.487.5 ≠=

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102

• Step 10 – Iterate on c until force equilibrium is satisfied

in.17.5=c0083.0=sε

ksi 06== ys ff

009.0=fdε

ksi 49.8=fef

( )( ) ( )( )( )( )( )( )in.120.786ksi50.928

ksi48.2in.0.96ksi60in.3.00 22 +=c

.Oin.5.17 Kc ==

The value of c selected for the final iteration is correct.

Design Example: Flexural Strengthening of an Interior Beam

0027.0=cε

786.01 =β

928.01 =α

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103

• Step 11 – Calculate reinforcement and FRP contribution to strength

ftkinkcdfAM ssns −=−=⎟⎠⎞

⎜⎝⎛ −=⎟

⎠⎞

⎜⎝⎛ −= 292504,3

2)17.5(786.05.21)60)(00.3(

21β

Design Example: Flexural Strengthening of an Interior Beam

ftkinkcdfAM ffefsf −=−=⎟⎠⎞

⎜⎝⎛ −=⎟

⎠⎞

⎜⎝⎛ −= 85017,1

2)17.5(786.024)2.48)(96.0(

21β

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104

• Step 11 – Calculate design flexural strength of the section

[ ] ( ) ftkMMM nfnsn −=+=+= 327)85(85.02929.0ψφφ

The strengthened section is capable of sustaining the new required moment strength

Design Example: Flexural Strengthening of an Interior Beam

The flexural strength is calculated using the reduction factor. Since εs =0.0083>0.005, the value of Ф is 0.9

ftkMftkM un −=≥−= 294327φ

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• Step 12 – Check service stresses in the reinforcing steel and the FRP

Calculate the elastic depth to the cracked neutral axis by summing the first moment of the areas of the transformed section.

Design Example: Flexural Strengthening of an Interior Beam

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106

• Step 13 – Check service stresses in the reinforcing steel and the FRP

⎟⎟⎠

⎞⎜⎜⎝

⎛+−⎟⎟

⎞⎜⎜⎝

⎛⎟⎠⎞

⎜⎝⎛++⎟⎟

⎞⎜⎜⎝

⎛+=

c

ff

c

ss

c

ff

c

ss

c

ff

c

ss E

EEE

dh

EE

EE

EE

EEk ρρρρρρ 2

2

343.0k =

( )( ) in. 7.37in. 21.50.343 ==kd

Design Example: Flexural Strengthening of an Interior Beam

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107

• Step 13 – Check service stresses in the reinforcing steel and the FRP

Calculate the stress level in the reinforcing steel:

( )

( ) ( )y

ffffss

sffbis

ss fkddkddEAkddkddEA

EkddkdhEAMf 8.0

33

3, ≤

−⎟⎠⎞

⎜⎝⎛ −+−⎟

⎠⎞

⎜⎝⎛ −

−⎥⎦

⎤⎢⎣

⎡⎟⎠⎞

⎜⎝⎛ −+

( )( ) OKksi 48ksi 600.80ksi 40.4, =≤=ssf

The stress level in the reinforcing steel is within the recommended limit

Design Example: Flexural Strengthening of an Interior Beam

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108

• Step 14 – Check creep rupture limit t service for the FRP

Calculate the stress level in the FRP:

fufbif

s

fsssf fE

kddkdd

EE

ff 55.0,, ≤−⎟⎟⎠

⎞⎜⎜⎝

⎛−

−⎟⎟⎠

⎞⎜⎜⎝

⎛= ε

OKksiksif sf 50)85)(55.0(60.5, =≤=

Design Example: Flexural Strengthening of an Interior Beam

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109

• Step 14 – Detailing Requirements

Detail the FRP reinforcement as follow:

1. Check that shear force at termination is less than shear force that causes end-peeling (estimate as 2/3 of concrete shear strength).

2. Terminate FRP at ldf (per Eq. 12.2) past cracking moment.a) If shear force is higher extend FRP beyond and/or use

FRP U-wraps.

Design Example: Flexural Strengthening of an Interior Beam