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Assessing the Damage Potential in
Pretensioned Bridges Caused by Increased
  Truck Loads Due to Freight Movements



               Robert J. Peterman, Ph.D., P.E.

     Martin K. Eby Distinguished Professor in Engineering
                   Kansas State University
Disclaimer
The contents of this report reflect the views of the
authors, who are responsible for the facts and the
accuracy of the information presented herein. This
document is disseminated under the sponsorship of the
U.S. Department of Transportation’s University
Transportation Centers Program, in the interest of
information exchange. The U.S. Government assumes no
liability for the contents or use thereof.
Other Contributors


     Steven F. Hammerschmidt, CE Dept.
     Dr. Weixin Zhao, MNE Dept.
     Dr. B. Terry Beck, MNE Dept.
     Dr. John Wu, Ph.D., IMSE Dept.
Overview
 •Introduction
 •Surface Strain Relief Method
 •Test Specimens
 •Finite-Element Models
 •Results
 •Conclusions
Introduction
•Many bridges are approaching their design life expectancy and/or
exposed to larger demands (10-15% are currently deficient).
•In order to accurately assess the condition of a prestressed
concrete bridge (highway or railroad), the remaining prestress force
level must be known.
•Time dependent losses decrease the prestress force in a member.
•The project’s goal was to develop an efficient, and inexpensive
way to determine the existing stress in a prestressed concrete
bridge member, thus the condition of these bridges can be
accurately assessed.
Surface Strain Relief
 Major Steps:
 2) Set up initial strain measurement device
    •Electrical resistance strain (ERS) gages
    •Laser speckle imaging (LSI) device
 3) Core or notch to relieve strain
 4) Measure elastic rebound of the concrete
 5) Relate rebound of the concrete to the average prestress
    force
Surface Strain Relief
Electrical Resistance Strain (ERS) Gages
•Gage length of 2”
•Epoxy used to mount gage to surface
•Gages protected with polyurethane
coating and microcrystalline wax
•Four pin terminal block was connected
to the lead wires attached to the strain
gage with silicone
Surface Strain Relief
Laser Speckle Imaging (LSI) Device
•Device developed at Kansas State University
•Images the speckle pattern produced by a laser reflection off the
surface which serves as the “fingerprint” of the location
•Subsequent images are related to the reference images and the
amount of displacement is calculated




        LSI Device with a 2” Gage Length           Speckle Pattern
Coring/Notching Procedure
•Used a 3” outside diameter dry coring diamond bit
•Used a 4.5” diameter dry diamond cutting wheel
•Core and notch temperature was monitored using a
non-contact thermometer
Procedure
•Locations were marked on the beam and gages attached
•All gages were initially set to zero microstrain or the LSI device was
used to take initial readings
•Coring guide was clamped into position on the surface of the beam or
layout lines were drawn on the beam with a distance of 3.5” between
notches
•Core locations were cored to an initial depth of ¾” and then 1”
•Notch locations were cut to an initial depth of 1” and then 1¼”
•There was a 10 minute delay between any increase in depth to allow the
entire location to reach equilibrium with the surrounding area
Coring Procedure
Notching Procedure
Calculating the Average Prestress
Force
•The relief strain is a positive or tensile strain so a sign change is
needed
•Relief stress related to the relief strain through Hooke’s Law
                    σ =ε·E
•The modulus of elasticity was determined in accordance with
ASTM C469 and by the load deflection response of the beam
Calculating the Average Prestress
Force
Test Specimens
Rectangle Beams                  Beam 1
•Cast in 2010
•Strands initially stressed to
202.5 ksi                        Beam 2
•Average 28-day compressive
strength: 7,440 psi
Test Specimens
T-Beams
•Cast in March of 2002
•Lightly reinforced in
longitudinal direction
•Strands initially stressed to
202.5 ksi
•Average 28-day compressive
strength: 7,040 psi
Finite Element Models
•Models created:
   •Varying depth of cores: 0.75”, 1”, and 1.25”
   •Varying notch depths, spacing, and lengths:       Length

       •Depths of 1”, 1.125”, 1.25”                            Depth

       •Spacing of 2.5”, 3”, and 3.5”
       •Lengths of 2”, 3”, and 4”       Pin Support

   •Beams restraint as a pinned, roller

                                                          Roller Support
Finite Element Models
Finite Element Models
Method of Determining Average Stress
Finite Element Models
Variable Core Depth
                                            Simpson's Rule      % Relieved
                      Core Depth (in)
                                        Calculated Stress (psi)   Stress
                           0.75                  -266              82%
                             1                    15               101%
                           1.25                  174               112%
Finite Element Models
Variable Notch Depth
                                                                  Simpson's Rule      % Relieved
                                           Notch Depth (in)
                                                              Calculated Stress (psi)   Stress
                                                  1                   -352.85            76%
                                                1.125                   3.97             100%
                                                1.25                  317.93             121%




*Spacing between notches 3.5” and length of notch 3”
Finite Element Models
Variable Notch Spacing

                                                                     Simpson's Rule       % Relieved
                                             Notch Spacing (in)
                                                                  Calculated Stress (psi)   Stress
                                                    2.5                   283.18             119%
                                                     3                     81.45             105%
                                                    3.5                   -352.85            76%




*Depth of notch is 1” and length of notch is 3”
Finite Element Models
Notches on T-Beams




 Core perpendicular      Core parallel to             Notch
       to web            bottom of beam


  *T-beam properties were the same as the rectangle beam models
Finite Element Models

                                        Simpson's Rule       % Relieved
                       Method
                                     Calculated Stress (psi)   Stress
                     Core Parallel            20.53             103%
                  Core Perpendicular         -23.22             97%
                        Notch                 64.85             109%
Results
 Surface Strain Results — Cores
 Beam 1a
   Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
    1          330               301             8.8%                314              4.8%
    2          331               298             10.0%               328              0.9%
    3          329               325             1.2%                361              -9.7%
    4          331               297             10.3%               332              -0.3%
                                           Avg. = +7.6%                         Avg. = -1.2%

 Beam 1b
   Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
    1          381               279             26.8%               351              7.9%
    2          381               309             18.9%               390              -2.4%
                                           Avg. = +22.9%                        Avg. = +4.5%
Results
 Surface Strain Results — Cores
 Beam 2a
   Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
    1          269               240             10.8%               290               -7.8%
    2          268               220             17.9%               254               5.2%
    3          268               250             6.7%                300              -11.9%
    4          268               261             2.6%                290               -8.2%
    5          269               224             16.7%               247               8.2%
                                           Avg. = +10.9%                        Avg. = -2.1%

 Beam 2b
   Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
    1          266               184             30.8%               235              11.7%
    2          268               236             11.9%                -                 -
    3          266               197             25.9%               219              17.7%
    4          268               273             -1.9%               278              -3.7%
                                           Avg. = +16.7%                        Avg. = +7.8%
Results
 Surface Strain Results — Notches
 Beam 1b
   Notch Theoretical (με) 1" Depth (με)   1" Percent Error 1.25" Depth (με) 1.25" Percent Error
     1            383              236         38.4%              323              15.7%
     2            383              200         47.8%              248              35.2%
     *3           382              310         18.8%              369              3.4%
     *4           384              293         23.7%              311              19.0%
 * Used LSI device to measure strain   Avg. = +32.1%                      Avg. = +18.3%

 Beam 2a
   Notch Theoretical (με) 1" Depth (με)   1" Percent Error 1.25" Depth (με) 1.25" Percent Error
     *1           268              288         -7.5%              316             -17.9%
     *2           268              303        -13.1%              323             -20.5%
 * Used LSI device to measure strain   Avg. = -10.3%                      Avg. = -19.2%

 Beam 2b
   Notch Theoretical (με) 1" Depth (με) 1" Percent Error 1.25" Depth (με) 1.25" Percent Error
     1            266              283         -6.4%            305             -14.7%
     2            266              327        -22.9%            352             -32.3%
     *3           268              240         10.4%            302             -12.7%
 * Used LSI device to measure strain   Avg. = -6.3%                     Avg. = -19.9%
Results
 Surface Strain Results — Cores
 T-beam 1
  Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
   1          118               104             11.9%               123              -4.2%
   2          118               101             14.4%               126              -6.8%
   3          122               103             15.6%               108              11.5%
   4          118               111             5.9%                113              4.2%
                                         Avg. = +1.2%                          Avg. = +1.2%
 T-beam 2
  Core   Theoretical (με) 3/4" Depth (με) 3/4" Percent Error   1" Depth (με)    1" Percent Error
   1          184               171             7.1%                180              2.2%
   2          186               117             37.1%               149              19.9%
   3          189                58             69.3%                71              62.4%
   4          188                61             67.6%                78              58.5%
 Core 3 and 4, Reinforcement present in core
Results
 Surface Strain Results — Notches

 T-beam 2
   Notch Theoretical (με) 1" Depth (με)   1" Percent Error 1.25" Depth (με) 1.25" Percent Error
     1            182              162         11.2%              206             -13.0%
     *2           182              144         20.7%              157              13.6%
     *3           188              142         24.5%              163              13.4%
     *4           183              162         11.5%              328             -79.2%
     *5           183              131         28.4%              321             -75.4%
 * Used LSI device to measure strain      Avg. = +19.3%                     Avg. = +18.3%
Conclusions
 •A 3” core bit used with a 2” strain gage resulted in an almost
 complete rebound of the surface strain when coring to a depth of
 1”, with an average error of less than 8%
 •A notch depth of 1”, spacing of 3.5” and length of 3” provides
 more varied results, with an average error of around 20%
 •The Laser Speckle Imaging device provided a quick and accurate
 way to measure the strain.
 •Multiple locations can be tested to reduce the overall error, and
 taking the average of 4 cores is recommended.
Conclusions
•Strain drift due to temperature change can be mostly eliminated by
allowing 10 minutes after coring and 5 minutes after notching.
•Finite element models successfully predicted the amount of
relieved strain similar to the experimental results, and could be
used to determine the optimal method for other geometries and
strand configurations.
•Reinforcement around the core area significantly affects the
measured relief strain, and steps should be taken to prevent coring
in the immediate vicinity of stirrups.
CREDITS


         A special thanks to our
Associate Director, Dr. Mustaque Hossain.




     Slide design © 2009, Mid-America Transportation Center. All rights reserved.

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Assessing the Damage Potential in Pretensioned Bridges Caused by Increased Truck Loads Due to Freight Movements (Phase I)

  • 1. Assessing the Damage Potential in Pretensioned Bridges Caused by Increased Truck Loads Due to Freight Movements Robert J. Peterman, Ph.D., P.E. Martin K. Eby Distinguished Professor in Engineering Kansas State University
  • 2. Disclaimer The contents of this report reflect the views of the authors, who are responsible for the facts and the accuracy of the information presented herein. This document is disseminated under the sponsorship of the U.S. Department of Transportation’s University Transportation Centers Program, in the interest of information exchange. The U.S. Government assumes no liability for the contents or use thereof.
  • 3. Other Contributors Steven F. Hammerschmidt, CE Dept. Dr. Weixin Zhao, MNE Dept. Dr. B. Terry Beck, MNE Dept. Dr. John Wu, Ph.D., IMSE Dept.
  • 4. Overview •Introduction •Surface Strain Relief Method •Test Specimens •Finite-Element Models •Results •Conclusions
  • 5. Introduction •Many bridges are approaching their design life expectancy and/or exposed to larger demands (10-15% are currently deficient). •In order to accurately assess the condition of a prestressed concrete bridge (highway or railroad), the remaining prestress force level must be known. •Time dependent losses decrease the prestress force in a member. •The project’s goal was to develop an efficient, and inexpensive way to determine the existing stress in a prestressed concrete bridge member, thus the condition of these bridges can be accurately assessed.
  • 6. Surface Strain Relief Major Steps: 2) Set up initial strain measurement device •Electrical resistance strain (ERS) gages •Laser speckle imaging (LSI) device 3) Core or notch to relieve strain 4) Measure elastic rebound of the concrete 5) Relate rebound of the concrete to the average prestress force
  • 7. Surface Strain Relief Electrical Resistance Strain (ERS) Gages •Gage length of 2” •Epoxy used to mount gage to surface •Gages protected with polyurethane coating and microcrystalline wax •Four pin terminal block was connected to the lead wires attached to the strain gage with silicone
  • 8. Surface Strain Relief Laser Speckle Imaging (LSI) Device •Device developed at Kansas State University •Images the speckle pattern produced by a laser reflection off the surface which serves as the “fingerprint” of the location •Subsequent images are related to the reference images and the amount of displacement is calculated LSI Device with a 2” Gage Length Speckle Pattern
  • 9. Coring/Notching Procedure •Used a 3” outside diameter dry coring diamond bit •Used a 4.5” diameter dry diamond cutting wheel •Core and notch temperature was monitored using a non-contact thermometer
  • 10. Procedure •Locations were marked on the beam and gages attached •All gages were initially set to zero microstrain or the LSI device was used to take initial readings •Coring guide was clamped into position on the surface of the beam or layout lines were drawn on the beam with a distance of 3.5” between notches •Core locations were cored to an initial depth of ¾” and then 1” •Notch locations were cut to an initial depth of 1” and then 1¼” •There was a 10 minute delay between any increase in depth to allow the entire location to reach equilibrium with the surrounding area
  • 13. Calculating the Average Prestress Force •The relief strain is a positive or tensile strain so a sign change is needed •Relief stress related to the relief strain through Hooke’s Law σ =ε·E •The modulus of elasticity was determined in accordance with ASTM C469 and by the load deflection response of the beam
  • 14. Calculating the Average Prestress Force
  • 15. Test Specimens Rectangle Beams Beam 1 •Cast in 2010 •Strands initially stressed to 202.5 ksi Beam 2 •Average 28-day compressive strength: 7,440 psi
  • 16. Test Specimens T-Beams •Cast in March of 2002 •Lightly reinforced in longitudinal direction •Strands initially stressed to 202.5 ksi •Average 28-day compressive strength: 7,040 psi
  • 17. Finite Element Models •Models created: •Varying depth of cores: 0.75”, 1”, and 1.25” •Varying notch depths, spacing, and lengths: Length •Depths of 1”, 1.125”, 1.25” Depth •Spacing of 2.5”, 3”, and 3.5” •Lengths of 2”, 3”, and 4” Pin Support •Beams restraint as a pinned, roller Roller Support
  • 19. Finite Element Models Method of Determining Average Stress
  • 20. Finite Element Models Variable Core Depth Simpson's Rule % Relieved Core Depth (in) Calculated Stress (psi) Stress 0.75 -266 82% 1 15 101% 1.25 174 112%
  • 21. Finite Element Models Variable Notch Depth Simpson's Rule % Relieved Notch Depth (in) Calculated Stress (psi) Stress 1 -352.85 76% 1.125 3.97 100% 1.25 317.93 121% *Spacing between notches 3.5” and length of notch 3”
  • 22. Finite Element Models Variable Notch Spacing Simpson's Rule % Relieved Notch Spacing (in) Calculated Stress (psi) Stress 2.5 283.18 119% 3 81.45 105% 3.5 -352.85 76% *Depth of notch is 1” and length of notch is 3”
  • 23. Finite Element Models Notches on T-Beams Core perpendicular Core parallel to Notch to web bottom of beam *T-beam properties were the same as the rectangle beam models
  • 24. Finite Element Models Simpson's Rule % Relieved Method Calculated Stress (psi) Stress Core Parallel 20.53 103% Core Perpendicular -23.22 97% Notch 64.85 109%
  • 25. Results Surface Strain Results — Cores Beam 1a Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 330 301 8.8% 314 4.8% 2 331 298 10.0% 328 0.9% 3 329 325 1.2% 361 -9.7% 4 331 297 10.3% 332 -0.3% Avg. = +7.6% Avg. = -1.2% Beam 1b Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 381 279 26.8% 351 7.9% 2 381 309 18.9% 390 -2.4% Avg. = +22.9% Avg. = +4.5%
  • 26. Results Surface Strain Results — Cores Beam 2a Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 269 240 10.8% 290 -7.8% 2 268 220 17.9% 254 5.2% 3 268 250 6.7% 300 -11.9% 4 268 261 2.6% 290 -8.2% 5 269 224 16.7% 247 8.2% Avg. = +10.9% Avg. = -2.1% Beam 2b Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 266 184 30.8% 235 11.7% 2 268 236 11.9% - - 3 266 197 25.9% 219 17.7% 4 268 273 -1.9% 278 -3.7% Avg. = +16.7% Avg. = +7.8%
  • 27. Results Surface Strain Results — Notches Beam 1b Notch Theoretical (με) 1" Depth (με) 1" Percent Error 1.25" Depth (με) 1.25" Percent Error 1 383 236 38.4% 323 15.7% 2 383 200 47.8% 248 35.2% *3 382 310 18.8% 369 3.4% *4 384 293 23.7% 311 19.0% * Used LSI device to measure strain Avg. = +32.1% Avg. = +18.3% Beam 2a Notch Theoretical (με) 1" Depth (με) 1" Percent Error 1.25" Depth (με) 1.25" Percent Error *1 268 288 -7.5% 316 -17.9% *2 268 303 -13.1% 323 -20.5% * Used LSI device to measure strain Avg. = -10.3% Avg. = -19.2% Beam 2b Notch Theoretical (με) 1" Depth (με) 1" Percent Error 1.25" Depth (με) 1.25" Percent Error 1 266 283 -6.4% 305 -14.7% 2 266 327 -22.9% 352 -32.3% *3 268 240 10.4% 302 -12.7% * Used LSI device to measure strain Avg. = -6.3% Avg. = -19.9%
  • 28. Results Surface Strain Results — Cores T-beam 1 Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 118 104 11.9% 123 -4.2% 2 118 101 14.4% 126 -6.8% 3 122 103 15.6% 108 11.5% 4 118 111 5.9% 113 4.2% Avg. = +1.2% Avg. = +1.2% T-beam 2 Core Theoretical (με) 3/4" Depth (με) 3/4" Percent Error 1" Depth (με) 1" Percent Error 1 184 171 7.1% 180 2.2% 2 186 117 37.1% 149 19.9% 3 189 58 69.3% 71 62.4% 4 188 61 67.6% 78 58.5% Core 3 and 4, Reinforcement present in core
  • 29. Results Surface Strain Results — Notches T-beam 2 Notch Theoretical (με) 1" Depth (με) 1" Percent Error 1.25" Depth (με) 1.25" Percent Error 1 182 162 11.2% 206 -13.0% *2 182 144 20.7% 157 13.6% *3 188 142 24.5% 163 13.4% *4 183 162 11.5% 328 -79.2% *5 183 131 28.4% 321 -75.4% * Used LSI device to measure strain Avg. = +19.3% Avg. = +18.3%
  • 30. Conclusions •A 3” core bit used with a 2” strain gage resulted in an almost complete rebound of the surface strain when coring to a depth of 1”, with an average error of less than 8% •A notch depth of 1”, spacing of 3.5” and length of 3” provides more varied results, with an average error of around 20% •The Laser Speckle Imaging device provided a quick and accurate way to measure the strain. •Multiple locations can be tested to reduce the overall error, and taking the average of 4 cores is recommended.
  • 31. Conclusions •Strain drift due to temperature change can be mostly eliminated by allowing 10 minutes after coring and 5 minutes after notching. •Finite element models successfully predicted the amount of relieved strain similar to the experimental results, and could be used to determine the optimal method for other geometries and strand configurations. •Reinforcement around the core area significantly affects the measured relief strain, and steps should be taken to prevent coring in the immediate vicinity of stirrups.
  • 32. CREDITS A special thanks to our Associate Director, Dr. Mustaque Hossain. Slide design © 2009, Mid-America Transportation Center. All rights reserved.

Editor's Notes

  1. The process of determining the average prestress force in the member by the surface strain relief method involves four major steps: 1) Setting up the initial strain measurement device whether it would be the use of Linear-resistance strain gages or the use of a Laser Speckle Imaging Device, then coring around the strain gage or cutting notches on each end of the strain gage or the area measured using the LSI device. Once the area is notched or cored the relaxation of the concrete is measured and then the measured strain relaxation can be used to calculate the average prestress force in the member.
  2. 2” Linear Strain gages were used due to the large size of aggregate present in many concrete mixes. The gages were attached to the beam using a low creep epoxy to minimize any error in the measurement. In order to core around the gage, the terminal wires needed to be disconnected so a four pin terminal block was attached to the gage after the gage had be protected with two protective layers; polyurethane coating and microcrystalline wax.
  3. Dr. Peterman, you know more about the Laser Speckle than I do so feel free to expand on what I have put on the slide
  4. A 3” outside diameter dry diamond coring bit show in the lower right picture was used for the coring method and a 4.5” diameter dry diamond cutting wheel attached to a hand held grinder fitted with a cutting and dust extraction guide was used for the notching method. To monitor the effect of temperature increases and correct for this a non-contact thermometer was used to measure the temperature throughout the process
  5. The gages were attached to the beam in a configuration as show in the figure with the gages aligned to the maximum strain in the beam and at the same height as the centriod of the prestressing steel
  6. Once the gage has been zeroed, the lead wires are disconnected at the terminal block and a coring guide is attached to the beam, as shown in the upper right photo, next using the coring bit and drill the gage is cored around as shown in the left figure. The lower right figure shows the gage once the process is complete
  7. The notching process is similar to the coring procedure with a few differences, the LSI device was used with the notching procedure to achieve a higher accuracy. In the upper left corner, the LSI device is mounted to the beam and initial reading taken. Then the LSI device is removed and the notches are cut as in the figure on the right side. After cutting the notches, the LSI device is reattached to the beam using the mounts attached to the beam and a measurement is take.
  8. The relief of strain is a positive or tensile strain due to the gage initially being set to zero strain, and then when the compression is relieved in the core or between the notches, a tensile or expanding strain is measured. To relate the relieved strain or residual stress, a sign change is needed to represent the compressive force in the beam
  9. Beam elements with an initial stress equal to the average prestress stress were used for the prestressing steel and structural hex elements were used for the remaining beam. Individual properties were given to the steel and the concrete used in the models. Each model consisted of approximately 15,000 elements, with a average mesh size of 1 inch for the majority of the model and a mesh size of .25 inch around the core or notch. This was done to reduce the computational time of each model. Red = Maximum Tensile Stress Orange = Approximate Zero Black = Maximum Compressive Stress
  10. To determine the measured relief strain from the finite element models, the strain values were plotted across the length of the core or notch then using Simpson’s Rule the measured strain was calculated across the area of where the gage would be positioned as shown in the figure.
  11. Three models were created with the only variable changing was the depth of core (3/4”, 1”, and 1 ¼” ) One inch core provided the closest to 100% relief of stress
  12. Next using the finite element models, various notch configurations were modeled
  13. Finite Element models were made using the optimal method determined from the rectangle beam models to compare the results, also the direction of the core was investigated
  14. The direction of core did not create a significant variation in the relieved stress, this was modeled due to the tapered web of the T-beams to see the error created if the core was not drilled parallel to the base of the beam Overall the relieved stresses were comparable to the rectangle beam models
  15. Beam 1a and 1b were casted at the same time, so theoretically each beam should have the same properties. Beam 1a was tested 3 months after casting while beam 1b was tested around 10 months after casting to compare the effect of time on the method.
  16. Beam 2a and 2b were casted at the same time, so theoretically each beam should have the same properties. Beam 2a was tested 3 months after casting while beam 2b was tested around 10 months after casting to compare the effect of time on the method. Core 2 on beam 2b was damaged while increasing the depth from ¾” to 1”
  17. The error with the notching procedure was generally larger (around 10% larger) than the coring procedure. The LSI device had smaller errors that the strain gages, due to the LSI device having a larger gage length so it captures more of the double hump as shown in the finite element models Beam 1a was not tested with the notching procedure due to lack of room on the beam and the amount of cores taking from the beam
  18. The T-beams had errors similar to beam 1b and 2b which were tested approximately 10 months after casting Reinforcement running through the core significantly effects the results of the core as shown in Cores 3 and 4 on T-beam 2
  19. Larger overall errors than with the coring method, similar to with the rectangle beams data Notch location 4 and 5 at a depth of 1.25” and error was seen with the LSI device making a larger error and were not used to compute the average prestress force in the beam as shown on the next slide
  20. This would be the last slide, click the text to change it to your information.