Saudconsult Presentation 2013

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    Modeling, Analysis and Design of Buildings AIT - Thailand ACECOM

    Bridges Saudi Arabia 2013

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    Modeling, Analysis and Design of Buildings AIT - Thailand ACECOM

    Bridges Saudi Arabia 2013

    1. General Overview.

    2. Problems Associated with Expansion Joints.

    3. Connection Types Between Precast Pre-stressed

    Bridge Girders Made Continuous Over Piers.

    4. Showcasing the Design of Continuous Decks Over

    Simple Spans Precast Pre-stressed Bridge Girders.

    5. Conclusions.

    6. References.

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    1. General Overview

    Bridges Saudi Arabia 2013

    On the other hand, the aforementioned expansion joints cause maintenance problems and consequent

    the durability of this type of bridges may be significantly improved by eliminating or reducing expansio

    joints in their decks. Therefore, this type of superstructure may be designed as a series of simple spans b

    their connections should be detailed for converting them to act as continuous spans for loads applied aft

    continuity is established.

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    1. General Overview (Contd.)

    Bridges Saudi Arabia 2013

    However, achieving continuity in bridge decks built

    using precast pre-stressed girders induces secondary

    stresses (shrinkage, creep, thermal stresses, etc.)

    that can cause structural damage of the decks, unless

    their analysis, design and construction have beenperformed properly.

    Therefore, this transformation of simple-span precast

    pre-stressed bridge girders to continuous spans, in

    view of the difficulty in assessing the long-term

    effects of time-dependent material behavior (aging,

    creep, and shrinkage), makes its design a challengingtask for ensuring the constructibility, safety,

    serviceability, and durability.

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    1. General Overview (Contd.)

    Bridges Saudi Arabia 2013

    Figure 1: Partial Continuity Detail Through

    Continuous Separated Slab

    Additionally, the detailed description and analysis

    results of Staged Construction (including timedependent material behavior effects) Finite Element

    Modeling of a case study of four-span simply

    supported precast pre-stressed bridge girders made

    continuous using continuous slab over piers, as

    shown in Figure 1 (partial continuity)2)

    and its

    proposed typical continuity connection details are

    presented and discussed.

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    2. Problems Associated with Expansion Joints.

    Bridges Saudi Arabia 2013

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    2. Problems Associated with Expansion Joints.

    Bridges Saudi Arabia 2013

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    Figure 3: Full Continuity Detail Method 2, Narrow In-situ Integra

    Crosshead [BA 57/01]2)

    Method 2: As shown in Figure 3, this method utilizes in-

    situ integral crosshead which may be designed to develop

    full continuity moments. The temporary supports are notrequired, permanent bearings may be in single or twin line

    and the continuity reinforcement is provided in the slab

    and at the bottom of bridge girders.

    3.1 Full Continuity Methods (Contd.)

    Figure 4: Full Continuity Detail Method 3, Integral Crosshead Castin Two Stages [BA 57/01]2)

    Method 3: As shown in Figure 4, this method utilizes in-

    situ integral crosshead which may be designed to develop

    full continuity moments. The girders are supported on

    stage 1 crosshead during erection. The crosshead is

    monolithic with pier and the continuity reinforcement is

    provided in the slab and at the bottom of girders.

    The above methods 2 and 3 are the most commonly used methods for achieving full continuity. Method 2

    has been extensively used in North America [BA 57/01]2).

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    AASHTO LRFD 20071) outlined design provisions for full continuity approach of bridges composed

    simple span precast girders made continuous and states that this approach has been used successfully

    several parts of the country. However, there are arguments about the effectiveness of this approach in casof composite bridge decks using precast pre-stressed girders. Partial continuity is generally preferred

    full continuity in such structures because of the difficulty in assessing the long-term effects of pre-stres

    induced deflection in full-continuity construction [BA 57/01]2).

    3.1 Full Continuity Methods (Contd.)

    Figure 5: Francis Case Memorial Bridge crosses the Washington Chan

    of the Potomac River in Washington, DC [Telang and Mehrabi]3)

    Additionally, the survey of using this bridge

    construction approach in some American States

    revealed that it could be accompanied with cracks ofunusual severity that can create a dangerous

    situation. This may be clarified through the following

    Bridge Case Study [Telang and Mehrabi]3).

    The Francis Case Memorial Bridge, carries eight

    traffic lanes over one channel of the Potomac River in

    Washington, DC, connecting the downtown with

    Potomac Park (Figure 5). In 1994 the approach spans

    of this bridge were replaced with precast pre-stressed

    concrete girders made continuous.

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    3.1 Full Continuity Methods (Contd.)

    Figure 6: One of the larger cracks [Telang and M

    In other words, by providing a large amount of positive moment

    reinforcement at the diaphragms, makes the diaphragm area stronger

    than the adjacent girder sections, thereby forcing the cracking to occurin far more critical but weaker areas of the girder span rather than in

    the region of diaphragm [Telang and Mehrabi]3).

    After four years, during a routine inspection, severe vertical cracks had been observed adjacent to th

    intermediate support at Pier B on eight interior pre-stressed girders. The observed cracks were most

    vertical, traversed the complete width of the bottom flange of the girder and, in some cases, traversed thfull girder height with the widest crack located at 1.4 m from the Pier (see Figure 6). Immediately all th

    girders that were cracked or showed imminent potential for similar distress had been shored to ensu

    safety of the structure. Then an in-depth research study had been initiated to ascertain the caus

    prognosis and whether the structure could be repaired [Telang and Mehrabi]3).

    Analytical investigation showed that the large positive moments generated on the Case Bridge that causin

    tensile stresses and cracking at the soffit of girders at intermediate supports were due primarily to threstraint provided by the positive moment reinforcement in continuity diaphragm and the reduce

    effectiveness of pre-stressing force at the end of the positive moment reinforcement within the girder cros

    section, thereby creating an unusually weak section susceptible to

    cracking under the applied moments.

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    3.1 Full Continuity Methods (Contd.)

    Therefore, the design of the full continuity approach should be

    attempted with caution for ensuring that the positive moment

    connection at continuity diaphragms being designed and detailedsuch that any cracking, if it occurs, should be formed in the positive

    moment region of diaphragm, rather than in the girder section [Telang

    and Mehrabi]3). However, this may not normally be ensured.

    It is worth mentioning that the four American States Florida, Georgia,

    Minnesota, and Texas, based on their past experience, are not using

    full continuity in the design for the precast pre-stressed concretegirder bridges [Chung C. Fu and Tarek Kudsi]6).

    After experiencing difficulty in attaining continuity, spalling concrete

    at the pier diaphragm, rotating at the end abutment (see Figures 7 and

    8), Florida and Texas abandoned the practice of continuity and are

    mainly designing simple span girder bridge [Chung C. Fu and Tarek

    Kudsi]6), or using a simply supported girders supporting a

    longitudinally continuous reinforced concrete deck over one to three

    interior supports, the latter method, is currently the standard in Texas

    [Scott Walton and Timothy E. Bradberry]4).

    Figure 7: Cracking of the Beam and Diaphragm at Th

    Intersection [Scott Walton and Timothy E. Bradberry

    Figure 8: Severely Cracked Beam Ends at Continuity

    Diaphragm [Scott Walton and Timothy E. Bradberry]4

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    Figure 9: Partial Continuity Detail Method 1

    Tied Deck Slab [BA 57/01]2)

    Method 1: This method of partial continuity shown in

    Figure 9, does not accommodate support rotations, there

    is no moment continuity between spans and could be

    susceptible to cracking. Separate bearings and end

    diaphragms are provided for each span, tie reinforcementat mid-depth of the slab is debonded for a short length

    either side of the joint to permit deck rotation.

    Additionally, the slabs between spans are separated

    using compressible joint fillers (but deck waterproofing

    and deck surfacing are continuous) and special seals

    are provided over the joint for double protection [BA

    57/01]2) .

    This type of continuity can be achieved over piers in bridge decks built using precast pre-stressed girder

    by providing continuity in the deck slab only. BA 57/01

    2)

    describes the following two possible methods foachieving the partial continuity.

    3.2 Partial Continuity Methods

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    Figure 10: Partial Continuity Method 2, Contin

    Separated Slab

    Method 2: This method of partial continuity shown in Figure 10, is similar in concept to the continuity det

    type 4, described by BA 57/012)

    . In this method, first the girders are erected upon the ledge of the inverted

    bent caps and the deck slab in each span will be casted separately and hence the bridge decks (at th

    construction stage) will act as a series of simple spans.

    3.2 Partial Continuity Methods (Contd.)

    Then the connecting slab, as shown in Figure 10, shall be

    casted after hardening of its adjacent deck slabs by a period

    of time as maximum as possible, in order to mitigate

    significantly the long-term effects of time dependent

    deformation in the connecting slab. Therefore, the minimumallowable duration for the above described period of time and

    the minimum girders age when casting the connecting slab

    should be specified in the design drawings.

    Additionally, the deck slab shall be separated from support

    girders for a short length (debonding horizontal length

    between vertical exterior edges of end diaphragms (as shownin Figure 10) using compressible material, in order to provide

    rotational flexibility.

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    This approach has been used successfully in Kingdom of

    Saudi Arabia and it is worth summarizing its advantages:

    This approach retains the simplicity and economy ofsimply supported construction whilst obtaining the

    various advantages of deck slab continuity [BA

    57/01]2).

    The various relative rotations and deflections at the

    support positions are accommodated within the

    connecting slab elements and there is moment

    continuity between spans.

    3.2 Partial Continuity Methods (Contd.)

    Figure 10: Partial Continuity Method 2, Continuous Separate

    Method 2 (Contd.): It is worth mentioning that the increasing of the aforementioned debonding lengt

    reduces the stiffness of the connecting slab and consequently, reduces its restraint/continuity momen

    However, the designer should carefully consider the instantaneous and long term effects of secondarstresses such as shrinkage, creep, thermal stresses, differential settlement, etc. (in terms of time an

    construction schedule) in assessing design issues such as tension/compression and bending moment

    developed in the connecting and in span slabs/ girders, bearing displacement, etc.

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    Method 2 (Contd.):On the other hand, this method of partial continuity

    has the following disadvantages:

    The amount of additional longitudinal

    reinforcement required in the slab/connecting

    slab to handle the negative and positive moments

    is significant/costly.

    The providing of proper span for connecting slab

    increases the eccentricity of bearing vertical

    reactions against its supporting bent pier and

    consequently additional amount of reinforcing

    bars and concrete will be required.

    3.2 Partial Continuity Methods (Contd.)

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    4. Showcasing the Design of Continuous Decks Over Simple Spans

    Precast Pre-stressed Bridge GirdersA case study of Bridge spanning over a floodplain along the proposed expressway (M.O.T, KSA

    connecting Al-Qassim Province with Makkah Al-Mukarramah, provides some guidelines anconsiderations that may be taken into account during the structural modeling and design of continuou

    decks over simple spans precast pre-stressed bridge girders.

    This case study bridge (as shown in Figure 11) carries eight traffic lanes and consists of (non-skewed

    twelve equal spans of about 30 m, composed of simply supported girders supported on ledges o

    inverted -T bent caps. Then each four spans are made continuous for superimposed / live loads throug

    a continuous cast in place concrete decks.

    Figure 11: Cross Section of Case Study Bridge

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    4.1 Modeling Development

    Figure 13: Proposed Continuity Detail

    Figure 12: Girder Cross Section

    Finite Element Models are used to investigate the most

    probable responses of continuous decks over theaforementioned four simple-spans precast pre-stressed

    (case study) Bridge girders due to vehicular live

    loads/superimposed dead loads, time dependent material

    behavior effects, thermal stresses, etc., using SAP 2000

    software package. Accordingly, a proposed continuity

    connection detail is presented and discussed.

    The case Bridge of four continuous spans is composed of

    23 Bulb Tee precast pre-stressed girders (see Figure 12)

    in each span and constant girder spacing and span of

    1710 mm and 27800 mm; respectively. Each girder is post-

    tensioned with two 2240 mm2 tendons, with a jacking

    force of 3130 kN per tendon and simply supported in both

    ends on the ledges of inverted -T bent caps through steelreinforced elastomeric bearings (see Figure 13).

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    4.1 Modeling Development (Contd.)

    Then the four simple spans of girders are converted to continuous

    spans through cast in place concrete slab of 200 mm thickness.

    However, the girder top surface within the connecting slab region isdropped by 150 mm to allow increasing of the connecting slab

    thickness to 330 mm and accommodating 20 mm thick of

    compressible filler, as shown in Figure 13.

    Expansion joints (see Figure 14) are provided at both ends of the

    aforementioned developed four continuous spans.

    Three-dimensional models are

    utilized with proper refinement

    of their components where

    required as shown in Figure 15.

    Figure 15: Finite Element Model (FEM) Plan

    Figure 14: Proposed Expansion Joint De

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    Therefore, each bearing is modeled using three spring elements distributed along transverse axis in

    perpendicular to girder centerline and connected together with its associated girder end (frame

    Element) by rigid link elements with their calculated fractional stiffness coefficients (see Figures 17and 18).

    Figure 17: Modeling of Bearings (A Set of Rigid

    Links and Springs)

    4.1 Modeling Development (Contd.)

    Figure 18: Modeling Connection between Deck

    Slab and Girder End Block

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    In developing the Finite Element Models, the application of the following loads and environmental effects are

    adopted:

    Self-weight of Structure.

    Superimposed Dead Loads. Vehicular Live Loads in accordance with M.O.T Highway Design Manual5).

    Uniform Temperature (TU) and Gradient Temperature (TG) in accordance with M.O.T Highway Design Manual5) .

    Differential Settlement of 25 mm of individual foundation in accordance with M.O.T Highway Design Manual5).

    Time Dependent material behavior effects of concrete and tendons.

    The Non-Linear Staged Construction Analysis has been adopted for the developed Finite Element Models in order to

    investigate the effect of construction scheduling, aging, shrinkage and creep. However, the material and geometric

    non-linearity are not considered and the following groups of elements, load patterns and load cases have beenadopted for defining the construction stages.

    4.1 Modeling Development (Contd.)

    Groups

    G1, G2, G3 and G4: for Girders in the first span through the fourth

    span.

    D1, D2, D3 and D4: for Diaphragms in the first span through the

    fourth span.

    S1, S2, S3 and S4: for Slabs in the first span through the fourth

    Span.

    L1, L2, and L3: for Connecting slabs throughout the four spans.

    Load Patterns

    TENDON: for pre-stressing applied to girders G1 through G4

    GRAVITY 1: for self weight of girders G1 through G4.

    GRAVITY2: for self weight of diaphragms in slabs S1 throug

    GRAVITY3: forself weight of slabs S1 through S4.

    GRAVITY4: for self weight of connecting slabs L1 through L

    GRAVITY5: for superimposed dead loads

    Vehicular Loads.

    Temperature loads (TU and TG).

    Settlement loads

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    Load Cases

    1. Load Case 1 (Starting from Zero Initial Condition) Add Girders G1, G2, G3 and G4 with an age 0 days

    Add Bearing for G1, G2, G3 and G4.

    Allow 10 days duration for aging and shrinkage.

    2. Load Case 2 (Continue from State at End of Load Case 1)

    Add Tendons

    Apply Tendon Load to G1, G2, G3 and G4.

    Apply Gravity 1 Load to G1, G2, G3 and G4.

    Allow 05 days duration for aging, shrinkage and creep.

    3. Load Case 3 (Continue from State at End of Load Case 2)

    Add Diaphragms for G1 through G4 with an age 0 days.

    Allow 05 days duration for aging, shrinkage and creep.

    4. Load Case 4 (Continue from State at End of Load Case 3)

    Apply Gravity 2 Load to the Diaphragms.

    Allow 05 days duration for aging, shrinkage and creep.

    4.1 Modeling Development (Contd.)

    Load Cases (Contd.)

    5. Load Case 5 (Continue from State at End of Load Case 4) Add S1, S2, S3 & S4 with an age of 0 days.

    Apply Gravity 3 Load to G1,G2, G3 & G4.

    Allow 60 days duration for aging, creep and shrinkage.

    6. Load Case 6 (Continue from State at End of Load Case 5)

    Add L1, L2 and L3 with an age of 0 days.

    Allow 14 days duration for aging, creep and shrinkage.

    7. Load Case 7 (Continue from State at End of Load Case 6)

    Apply Gravity 4 Load to Connecting Slabs.

    Apply Gravity 5 Load to all.

    8. Load Case 8 (Continue from State at End of Load Case 7)

    Allow 30 days duration for aging, shrinkage and creep.

    9. Load Case 9 (Continue from State at End of Load Case 8)

    Allow 300 days duration for aging, shrinkage and creep.

    10 Load Case 10 (Continue from State at End of Load Case 9)

    Allow 3000 days duration for aging, shrinkage and creep.11. Load Case 11 (Continue from State at End of Load Case 10)

    Apply vehicular loads (Maximum Positive Bending Moment)

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    (Load Cases, Contd.)

    12 Load Case 12 (Continue from State at End of Load Case 10) Apply Temperature Gradient (Maximum Positive Bending

    Moments).

    13 Load Case 13 (Continue from State at End of Load Case 10)

    Apply Temperature Uniform (Maximum Positive Bending Moments).

    14. Load Case 14 (Continue from State at End of Load Case 10)

    Apply Differential Settlement (Maximum Positive Bending Moment).

    15. Load Case 15 (Continue from State at End of Load Case 7)

    Apply vehicular loads (Maximum Negative Bending Moment)16. Load Case 16 (Continue from State at End of Load Case 7)

    Apply Temperature Uniform (Maximum Negative Bending Moment)

    17. Load Case 17 (Continue from State at End of Load Case 7)

    Apply Differential Settlement (Maximum Negative Bending

    Moments)

    4.1 Modeling Development (Contd.)

    However, additional load cases for modeling the effect of increasing the time period between casting of the connectslab and its adjacent in-span deck slab to 10 and 180 days have been investigated, then load combinations have b

    also considered as appropriate.

    Figure 19: TYPICAL LOAD CASE DESCRIPTION FOR STAGES

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    4.2 Modeling Results and Discussions

    The main results that can be extracted from the described Finite Element Models and that are of

    interest for this study are:

    Forces/moments in frame/shell elements

    Top/bottom fiber stresses in shell elements

    Forces/displacement/rotation in spring/node elements

    However, the results and discussion herein will be concentrated on the structural performance of the

    connecting slab under the aforementioned applied loads/displacement/temperature/construction

    schedule.A space is not taken to provide the model results of the flexural moments and axial forces acting on

    the connecting slabs, however, its combination effects may be reflected by their resulting top and

    bottom fiber stresses.

    Therefore, the output results in terms of the top and bottom fiber stresses of connecting slab are

    selected as a compromise between accuracy and ease of study and comparison considerations. Theoutput results shall be denoted by their specified load case numbers as described in the model

    development, unless otherwise specified.

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    4.2 Modeling Results and Discussions (Contd.)

    A. Material Behavior Time Dependent Effects: This effect may be described by the top and bottom fi

    stresses of connecting slab as shown in Figures 20 through 23 (load cases nos. 7 and 10).

    Figures 20 and 21 show the top and bottom fiber stresses; respectively, of connecting slab upon hardening and applying of the permanent loads, while Figures 22 and 23 showing (respectively) t

    changing occurred in these fiber stresses in the long run (over 9 years) due to the effects of ti

    dependent deformation caused by shrinkage and creep.

    It can be noticed that the (instantaneous) maximum top fiber tensile stresses of 0.53 MPa and bottom fi

    compressive stresses of -0.42 MPa, switch their places under the long-term effect of shrinkage and cre

    and become -2.85 MPa (compression) and 3.25 MPa (tension); respectively.

    Figure 20: Top Fiber Stresses of Connecting Slab at End of Load Case 7

    Max. Stress = 0.53 MPa

    Figure 21: Bottom Fiber Stresses of Connecting Slab at End of Load Cas

    Max. Stress = -0.42 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    Accordingly, for design purposes, the state of fiber stresses shown in Figures 20/21 and Figures 22/2

    may be treated as the datum stresses for accumulating the extreme initial and long-term fiber stresse

    respectively, resulting from other load cases.

    In other words, the stresses resulting from load case causing tensile stresses on the top fiber

    connecting slab to be added to the stress datum shown by Figures 20 and 21 (short-term effect), and t

    stresses resulting from load case causing tensile stresses on bottom fiber of connecting slab to be adde

    to stress datum shown by Figures 22 and 23 (long-term effect).

    A. Material Behavior Time Dependent Effects (Contd.)

    Figure 22: Top Fiber Stresses of Connecting Slab at End of Load Case 10

    Max. Stress = -2.85 MPa

    Figure 23: Bottom Fiber Stresses of Connecting Slab at End of Load Cas

    Max. Stress = 3.25 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    B. Vehicular Live Loads Effect: This effect may be

    described by the top and bottom fiber stresses of the

    connecting slab shown in Figures 24 through 27 (LoadCases Nos. 15 and 11).

    Figure 24 shows the maximum top fiber tensile

    stresses of the connecting slab due to vehicular load

    (that applied in the locations developing maximum

    negative moments on the connecting slab) plus its

    existing (instantaneous) fiber tensile stress due topermanent loads. It can be seen that the maximum top

    tensile stresses has been increased from 0.53 MPa

    (see Figure 20) to about 4.0 MPa. This increasing in the

    tensile stresses in the connecting slab due to

    vehicular loads is exceeding 6 times its existing

    (instantaneous) tensile stresses due to permanentloads. While Figure 25 shows the corresponding

    bottom fiber compressive stresses.

    Figure 24: Top Fiber Stresses of Connecting Slab at End of Load Case

    Max. Stress = 4.00 MPa

    Figure 25: Bottom Fiber Stresses of Connecting Slab at End of Load Ca

    Max. Stress = -3.90 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    B. Vehicular Live Loads Effect (Contd.): Figure 27

    shows the maximum bottom tensile stresses of the

    connecting slab due to vehicular loads (applied on

    the connecting slab span for developing maximum

    positive moment on it) plus its existing (long-term)

    fiber tensile stresses due to permanent loads. It

    can be seen that the maximum bottom tensile

    stresses has been increased from 3.25 MPa (see

    Figure 23) to about 5.0 MPa. This increasing in the

    tensile stresses in the connecting slab due to

    vehicular loads is about 50% of its existing (long-

    term) tensile stresses due to permanent loads.

    While Figure 26 shows the corresponding top fiber

    compressive stresses.

    Figure 26: Top Fiber Stresses of Connecting Slab at End of Load Case 11

    Max. Stress = -4.50 MPa

    Figure 27: Bottom Fiber Stresses of Connecting Slab at End of Load Case

    Max. Stress = 5.00 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    C. Temperature Gradient Effects: This effect (based on the differential thermal gradient recommended b

    M.O.T, KSA)5) causes tensile stresses in the bottom fiber of the connecting slab, and therefore has bee

    added to the long-term stresses ofpermanent loads as shown in Figure 29 (at the end of load case 12and the corresponding top fiber compressive stresses as shown in Figure 28.

    It can be seen that the maximum bottom fiber tensile stresses developed due to the effect of therma

    gradient plus long-term effect of permanent load is increased from 3.25 to about 16.50 MPa that exceedin

    the top and bottom tensile stresses resulting from the effect of vehicular live loads shown in Figures 2

    and 27; respectively.

    Figure 28: Top Fiber Stresses of Connecting Slab at End of Load Case 12

    Max. Stress = -16.50 MPa

    Figure 29: Bottom Fiber Stresses of Connecting Slab at End of Load Cas

    Max. Stress = 16.50 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    D. Differential Settlement Effects: This effect of differential settlement of 25 mm (M.O.T, KSA)5), may b

    described by the top and bottom fiber stresses of connecting slab shown in Figures 30 through 33 (End

    Load Cases Nos. 17 and 14). As shown in Figure 30, the maximum top fiber tensile stresses developed duto the specified value of differential settlement (that develops negative moment on the top fiber of th

    connecting slab) in the connecting slab plus its existing (instantaneous) fiber stress due to permane

    loads, is increased from 0.53 MPa to about 2.50 MPa. This increasing in the tensile stresses due to th

    specified differential settlement is exceeding three times the existing (instantaneous) tensile stresses du

    to permanent loads and equals about 55% of the vehicular load effect (see Figure 24) . While Figure 3

    shows the corresponding bottom fiber compressive stresses .

    Figure 30: Top Fiber Stresses of Connecting Slab at End of Load Case 17

    Max. Stress = 2.50 MPa

    Figure 31: Bottom Fiber Stresses of Connecting Slab at End of Load Case

    Max. Stress = -2.30 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    D. Differential Settlement Effects (Contd.):

    As shown in Figure 33, the maximum bottom fiber tensile stresses of connecting slab due to the specifievalue of differential settlement (that develops positive moment on the connecting slab) plus its long-ter

    fiber stresses of permanent loads is increased from 3.25 MPa to 5.50 MPa. This increasing in the tensi

    stresses in the connecting slab due to the specified differential settlement is about 70% of its existin

    (long-term) tensile stresses due to permanent loads and exceeding the effect of vehicular load (see Figu

    27). While Figure 32 shows the corresponding top fiber compressive stresses.

    Figure 32: Top Fiber Stresses of Connecting Slab at End of Load Case 14

    Max. Stress = -5.00 MPa

    Figure 33: Bottom Fiber Stresses of Connecting Slab at End of Load Cas

    Max. Stress = 5.50 MPa

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    4.2 Modeling Results and Discussions (Contd)

    E. Uniform Temperature Effects (Contd.): As shown in Figure 37, the maximum bottom fiber tensil

    stresses of the connecting slab after raising the uniform temperature by the specified value (plus it

    existing long-term top fiber tensile stresses due to permanent loads) is increased from 3.25 MPa (se

    Figure 23) to 3.50 MPa. This increasing in the tensile stresses in the connecting slab due to the specifieraising value of uniform temperature is about 7% of its existing (long-term) tensile stresses due t

    permanent loads and equals about 14% of the vehicular load effect (see Figure 27).

    It is worth mentioning that the uniform temperature applied could develop horizontal shear forces o

    bridge deck elastomeric bearings and since the location of bridge bearings off the neutral axis of th

    connecting slab, flexural moments in addition to axial forces will be developed in the connecting slab as

    result of this loading.

    Figure 36: Top Fiber Stresses of Connecting Slab at End of Load Case 13

    Max. Stress = -3.30 MPa

    Figure 37: Bottom Fiber Stresses of Connecting Slab at End of Load Cas

    Max. Stress = 3.50 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    F. Effect of Time Period Between Casting of Connecting Slab and its Adjacent in-span Slabs: The top

    and bottom fiber stresses shown in Figures 20 through 37 are based on allowing time period of 60 days

    between casting of connecting slab and its adjacent in-span slabs and corresponding age of girders of

    85 days when casting the connecting slab.

    Figures 38 and 39 show the estimated top and bottom fiber stresses of the connecting slab due to the

    long-term effects of permanent loads (over 9 years) when reducing the above described time period to

    10 days and 35 days age of girders when casting the connecting slab; respectively.

    On the other hand, the corresponding top and bottom fiber stresses of connecting slab due to long-

    term effects of permanent loads (over 9 years) when increasing the aforementioned time period to 180

    days (and corresponding age of girders to 200 days when casting the connecting slab) are shown in

    Figures 40 and 41.

    As can be seen from Figures 39 and 41, in the latter case, the maximum bottom fiber tensile stress of

    the connecting slab has been reduced from 4.00 MPa to 2.30 MPa (about 43%). Therefore, increasing of

    the above described period of time seems to be advantageous. This may be attributed to mitigation of

    the long-term effects of time dependent deformation caused by shrinkage and creep.

    Similarly, it may be concluded that the bottom fiber tensile stresses of connecting slab depends also on

    the girder age at time of casting of connecting slab and it would be reduced with using older girder age.

    4 2 M d li R lt d Di i (C td )

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    4.2 Modeling Results and Discussions (Contd.)

    F. Effect of Time Period Between Casting of Connecting Slab and its Adjacent in-span Slabs (Contd.):

    Figure 38: Top Fiber Stresses of Connecting Slab at End of Load Case 10a

    Max. Stress = -3.50 MPa

    Figure 39: Bottom Fiber Stresses of Connecting Slab at End of Load Case

    Max. Stress = 4.00 MPa

    Figure 40: Top Fiber Stresses of Connecting Slab at End of Load Case 10b

    Max. Stress = -1.94 MPa

    Figure 41: Bottom Fiber Stresses of Connecting Slab at End of Load Case

    Max. Stress = 2.30 MPa

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    4 2 Modeling Res lts and Disc ssions (Contd )

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    4.2 Modeling Results and Discussions (Contd.)

    G. Top and Bottom Fiber Stresses of Connecting Slab Due to (Un-factored) Combination of Loads.

    Figure 42: Top Fiber Tensile Stresses (Combination of Loads)

    Max. Stress = 6.30 MPa

    Figure 43: Corresponding Bottom Fiber Stresses (Combination of Loads

    Max. Stress = -6.00 MPa

    Figure 44: Bottom Fiber Tensile Stresses (Combination of Loads)

    Max. Stress = 12.80 MPa

    Figure 45: Corresponding Top Fiber Stresses (Combination of loads)

    Max. Stress = -12.80 MPa

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    4.2 Modeling Results and Discussions (Contd.)

    G. Load Combination Results (Contd.):

    And, the extreme (maximum) Bottom and top fiber stresses of the continuity slab using the above

    mentioned Service (I) load combination but taken 100% of the force effects of Temperature gradient(when live load is not considered) are equal to 17.60 and -17.80 MPa, as shown in Figures 46 and 47;

    respectively. It can be seen that the later combination of load is more critical.

    In view of all the above, (for design purposes), it may conclude that the bottom fiber (tensile) stresses

    of the connecting slab is more critical than its top fiber tensile stresses. This is an evidence that the

    increasing of time period between casting of continuity slab and its adjacent in-span slabs (for

    reducing the (long-term) bottom fiber tensile stresses (as shown in Figures 39 and 41) is advantageous.

    Figure 46: Bottom Fiber Tensile Stresses (Combination of Loads)

    Max. Stress = 17.60 MPa

    Figure 47: Corresponding Top Fiber Stresses (Combination of loads)

    Max. Stress = -17.80 MPa

    4 3 P d C ti it Sl b C ti D t il

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    4.3 Proposed Continuity Slab Connection Detail

    Figure 48: Continuity Detail over Piers

    A. Top Reinforcement: As shown in Figures 48

    through 49, the negative moment connection

    reinforcement of connecting slab shall be made

    with the reinforcement protruded from its adjacentin-span deck slab ends (that has been already

    casted and hardened) and extended (from both in-

    span slab ends) throughout its full span, and

    embedded there using 180o standard hook and

    anchoring bar with a diameter equal to or greater

    than the diameter of its negative moment

    reinforcement.

    The connecting slab connection detail has been proposed in view of its staged construction analy

    results, the design provisions specified by AASHTO LRFD 20071) (for the positive and negative mom

    connection reinforcement details of full continuity connection), and for ensuring that its top and bottreinforcement being adequately anchored/spliced with its adjacent deck slab/girder/end diaphra

    reinforcement (in order to assure its full design capacity throughout its span).

    4 3 P d C ti it Sl b C ti D t il (C td )

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    4.3 Proposed Continuity Slab Connection Detail (Contd.)

    Additionally, the aforementioned protruded negative

    moment reinforcement shall be extended into the in-

    span deck slabs, lap spliced with the deck slablongitudinal top reinforcement in compression zone

    and its termination to be staggered.

    B. Bottom Reinforcement: As shown in Figures 49 and

    50, the positive moment connection reinforcement of

    connecting slab shall be made using bottom

    reinforcing bars extended throughout its span andembedded into its adjacent end diaphragms (within

    the end diaphragm span region as shown in Figure

    49) or supporting on the girder ends (within girder

    width region as shown in Figure 50) using 180o

    standard hook and anchoring bar with a diameter

    equal to or greater than the diameter of its positive

    reinforcement.

    Figure 50: Continuity Detail over Piers (within girder width regio

    Figure 49: Continuity Detail over Piers (within end diaphragm spa

    4 3 P d C ti it Sl b C ti D t il (C td )

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    4.3 Proposed Continuity Slab Connection Detail (Contd.)

    Additionally, steel reinforcing bars equal in diameter and spacing to the positive moment connection

    reinforcement of connecting slab shall be protruded from the girder ends (at the same level of

    connecting slab bottom reinforcement as shown in Figures 48 and 50) and to be lap spliced with thebottom reinforcement of connecting slab.

    These protruded reinforcing bars shall be extended into the precast pre-stressed girder and to be

    (noncontact) lap spliced with its top reinforcing bars and their termination to be staggered in pairs

    symmetrical about its centerline.

    Figure 50: Continuity Detail over Piers (within girder width region)Figure 48: Continuity Detail over Piers

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    5. Conclusions

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    6. References

    Bridges Saudi Arabia 2013

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