Submitted:
22 February 2025
Posted:
25 February 2025
You are already at the latest version
Abstract
Keywords:
1. Introduction
- Increasing Load resistance.
- Increasing of bending moment capacity.
- Better deflection control.
- Increasing the stiffness of prestressed concrete I-bridge girders.
- Decrease in construction costs.
2. Experimental Program
2.1. Size and Shape of the Test Specimens
2.2. Prestressing and Reinforcement Detail
2.3. Concrete Mix Specification
2.4. Preparation of the Test Specimens
2.5. Experimental Variables
2.6. Test Setup and Instrumentation
2.7. Experimental Procedure
- The load cell and LVDTs were connected to the data logger to obtain the real time load, strains and displacement of the specimens as applied load increases see .
- Connect the data logger to the computer. The data was automatically recorded and stored utilizing the computerized data acquisition system.
- Loosen the load adjustment control wheel as to prevent any sudden application of load to the specimen.
- Slowly and steadily tighten the load adjustment control wheel after the specimen is placed properly on the testing rig specimens were loaded.
- The load control method was used during the test, the load was applied at an average rate of 90 kN/min during the linear elastic stage. As the cracks developed and, thus, the concrete had a plastic behavior, the digital load indicator was not showing a constant loading rate anymore.
- Because of the safety concern, the test was terminated when the specimens remind in a state where the load would be remain constant or slightly decrease and when the displacement was significantly increased. The tests was take an average period of 16 minute from beginning of loading process until the test was terminated.
- Hold the load adjustment control wheel and highlight the crack with line and mark each of the crack.
- Loosen the load adjustment control wheel before turning of the machine and disconnect if from the computer.
3. Expemental Results and Discusions
3.1. Tested Specimens
3.2. Load-Deflection Curves
3.3. Crack Patterns and Mode of Failure
4. Conclusion
- The flexural destruction of unbounded prestress concrete bridge i-girders experience elastic, elastic-plastic and ductility stages, similar to bounded prestress concrete bridge i-girders. Unbounded prestress concrete bridge I-girder present superior ductility and deformation-recovery ability after unloading.
- The tendon profile layout has a significant influence on the destruction process in unbounded prestress concrete bridge I-girders.
- The experimental results showed that the flexural behavior of tested specimens is divided in to three stages: elastic stage, elastic-plastic stage and plastic stage. All specimens exhibit flexural failure.
- The ultimate load of specimens using trapezoidal tendon profile, showed a maximum increased by 28.02 KN with increasing rate 7.81% for the specimen GF-3 TR if we compared it with control beam.
- The ultimate load of specimens using parabolic tendon profile had maximum increased by 49.6 KN with increasing rate 13.83% for the specimen GF-6 PR if we compared it with control beam.
- The ultimate load of specimens using harped tendon profile had maximum increased by 75.3 KN with increasing rate 20.99% for the specimen GF-2 HA if we compared it with control beam.
- The deflection of specimens using trapezoidal tendon profile, the specimen GF-3 TR had minimum vertical deflection 32.36 mm, which lesser than control beam by 4.44 mm with decreasing rate 12.07 % from control beam.
- The deflection of specimens using parabolic tendon profile, the specimen GF-5 PR had minimum vertical deflection 35.22 mm, which lesser than control beam by 1.58 mm with decreasing rate 4.29 % from control beam.
- The deflection of specimens using parabolic tendon profile, the specimen GF-2 HA had minimum vertical deflection 35 mm, which lesser than control beam by 1.80 mm with decreasing rate 4.89 % from control beam.
- Each tendon profiles shapes (trapezoidal, parabolic, harped) with eccentricity at end (ee)=0, had maximum ultimate load capacity. It’s can be concluded that specimen GF-9 HA with harped tendon profile had maximum ultimate load capacity from all other specimens. Also it’s can be concluded that specimen GF-3 TR with trapezoidal tendon profile had minimum deflection from all other specimens which agree with the result of finite element analysis by Ansys and Sap software, that done by Dixit and Naser[27,28]. These enhancement in specimens stiffness, ultimate loads capacities and deflections because of effect of tendon profile layout on flexural capacity of girders.
- The experimental results of tests on girders with optimized tendon profiles illustrated remarkable improvements in performance. These girders carried higher loads with less deflection than control beam. The efficiency of prestressing forces throughout the girder length makes the girders with optimized tendon configurations more performant. This allows for a more even distribution of the induced stresses to the concrete member, engaging more of the cross section for load carrying. This uniform stress distribution enhances ductility of the girder and hence the service life of the structure.
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
References
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| Type | Diameter (mm) | Area (mm2) |
Yield stress (Mpa) |
Ultimate Strength (Mpa) |
Maximum Elongation (%) |
Modulus Of Elasticity (Mpa) |
|---|---|---|---|---|---|---|
| strand | 15.26 | 140.54 | - | 2018 | 4.28 | 196,370 |
| Deformed bar | 11.74 | 108.28 | 595 | 673 | 20 | 200,000 |
| Deformed bar | 9.857 | 76.31 | 610 | 696 | 21 | 200,000 |
| Cement (g) |
Water (L) |
Additive (L) |
Fine Aggregate (kg) |
Coarse Aggregate (kg) |
W/C | Slump (mm) |
Maximum Aggregate Size (mm) |
|---|---|---|---|---|---|---|---|
| 425 | 160 | 4 | 880 | 910 | 0.38 | 150-180 | 19 |
| Specimen name | Tendon Profile name | Tendon Profile layout, units in (mm) |
|---|---|---|
|
GF-1 ST Control Beam |
Straight Tendon Profile With e = 180 mm |
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| GF-2 TR | Trapezoidal Tendon Profile With ee = + 80 mm |
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| GF-3 TR | Trapezoidal Tendon Profile With ee = 0 mm |
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| GF-4 TR | Trapezoidal Tendon Profile With ee = - 80 mm |
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| GF-5 PR | Parabolic Tendon Profile With ee = +80 mm |
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| GF-6 PR | Parabolic Tendon Profile With ee = 0 mm |
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| GF-7 PR | Parabolic Tendon Profile With ee = - 80 mm |
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| GF-1 HA | Harped Tendon Profile With ee = + 80 mm |
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| GF-2 HA | Harped Tendon Profile With ee = 0 mm |
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| GF-3 HA | Harped Tendon Profile With ee = - 80 mm |
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| Specimen Name |
First Crack Load (KN) |
First Crack Deflection (mm) |
Ultimate Load (KN) |
Ultimate Load Deflection (mm) |
Pcr/Pu % |
Failure Mode |
| PCR | ∆CR | Pu | ∆u | |||
| GF-1 ST | 142.60 | 0.95 | 358.70 | 36.80 | 39.75% | Flexural a,b |
| GF-2 TR | 122.02 | 0.96 | 371.63 | 36.76 | 32.83% | Flexural a,b |
| GF-3 TR | 154.12 | 1.42 | 386.72 | 32.36 | 39.85% | Flexural a,b |
| GF-4 TR | 95.80 | 0.79 | 351.27 | 35.24 | 27.27% | Flexural a,b |
| GF-5 PR | 131.72 | 1.16 | 383.75 | 35.22 | 34.32% | Flexural a,b |
| GF-6 PR | 80.00 | 1.11 | 408.30 | 39.56 | 19.59% | Flexural a,b |
| GF-7 PR | 119.1 | 0.85 | 398.98 | 37.83 | 29.85% | Flexural a,b |
| GF-1 HA | 150.45 | 1.52 | 426 | 35.74 | 35.32% | Flexural a,b |
| GF-2 HA | 151.03 | 1.20 | 434.00 | 35.00 | 34.80% | Flexural a,b |
| GF-3 HA | 139.02 | 1.20 | 409.00 | 37.90 | 33.99% | Flexural a,b |
| Compared Specimen | Increase in Ultimate Load | Decrease in Ultimate Load | Increase In Ultimate Load Deflection | Decrease In Ultimate Load Deflection | ||||
|---|---|---|---|---|---|---|---|---|
| (KN) | % | (KN) | % | (mm) | % | (mm) | % | |
| GF-1 ST & GF-2 TR | 12.93 | 3.60% | - | - | - | - | 0.04 | 0.11% |
| GF-1 ST & GF-3 TR | 28.02 | 7.81% | - | - | - | - | 4.44 | 12.07% |
| GF-1 ST & GF-4 TR | - | 7.43 | 2.07% | - | - | 1.56 | 4.24% | |
| GF-1 ST & GF-5 PR | 25.05 | 6.98% | - | - | - | - | 1.58 | 4.29% |
| GF-1 ST & GF-6 PR | 49.6 | 13.83% | - | - | 2.76 | 7.50% | - | |
| GF-1 ST & GF-7 PR | 40.28 | 11.23% | - | - | 1.03 | 2.80% | - | |
| GF-1 ST & GF-1 HA | 67.3 | 18.76% | - | - | - | - | 1.06 | 2.88% |
| GF-1 ST & GF-2 HA | 75.3 | 20.99% | - | - | - | - | 1.8 | 4.89% |
| GF-1 ST & GF-3 HA | 50.3 | 14.02% | - | - | 1.1 | 3% | - | - |
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