Title: Full-scale Reflective Cracking Test Update
1Full-scale Reflective Cracking Test Update
- Presented to FAA Airport Pavement
- Working Group Meeting
- By Hao Yin, Ph.D., P.E.
- Gemini Technologies, Inc.
- Date April 24, 2012
2Acknowledgement
- SRA
- Chuck Teubert
- Jerry Connelly
- Renaldo Aponte
- Jeff Stein
- Gupta Durgesh
- David Traverzo
- Pochtar Daniel
- Bing Xiao
- Henry Fermin
- FAA
- Dr. Satish Agrawal
- Dr. Gordon Hayhoe
- Donald Babargallo
- Ryan Rutter
- Frank Petch
- Murphy Flynn
- RMD
- Roy McQueen
- Christopher Deker
3Objective
Generate information from full-scale tests
(NAPTF) to assist in the improvement of current
design procedures for AC overlay on rigid airport
pavements.
4Scope
Evaluate the initiation and propagation of
bottom-up reflection cracks due to temperature
effect acting alone (thermally induced fatigue),
assuming intact PCC slabs.
Nunn, M., 1st RILEM 1989
5Key Parameters
1. Pavement Temperature T32oF, DT17oF
6Key Parameters
2. Horizontal Displacement at Joint 15 mils
7Key Parameters
3. Loading Rate ? 4. AC-PCC Interface Bond ?
8Progress Since 2011
- Laboratory tests
- Construction, instrumentation, and data
collection - Temperature Effect Simulation System (TESS)
tune-up and enhancements - Trial test
9Texas Overlay Tester
Determination of Loading Rate
Temp 32 oF Max Hori Dip 15 mils Loading Rate
0.25, 0.50, 1.0 mil/sec
10Overlay Tester Results
11Interface Bond Experiment
12Bond Strength Test
Temp 32 oF Loading Rate 0.05 mil/sec
13Bond Strength Test
14Bond Strength Test
15Temperature Unit Re-design
16Pavement Construction
17Pavement Construction
18Pavement Construction
19Pavement Construction
20Instrumentation Layout
South
1.5
ASG/CSG
ASG/CSG
L
T
L
L
12.0
Surface SG
T
ASG/CSG
ASG/CSG
L
L
T
L
ASG/CSG
ASG/CSG
T
T
T
T
1.5
North
21Data Collection
22 Mishap Before Overlay
North
South
23 Mishap After Overlay
E
Force, 92,000 lb
Force -85,000 lb
Ten
Com
N
S
56 mil
-46 mil
W
24 Mishap After Overlay
E
Com
N
S
Ten
W
25 Mishap After Overlay
26Crack Arrester
27Trial Test
- Feb 27 March 15
- AC/PCC interface temperature 32oF
- Max Hori Dis 0.015 in
- 600 sec per cycle
- 144 cycles per day
- Total of 2641 cycles
28Hydraulic Control
29Hydraulic Control Cont.
30Hori Dis Along Joint
North
South
31Pavement Temperature
32Crack Development36 Cycles
33Crack Development180 Cycles
34Crack initiation
35Dynamic Modulus
36Tensile Strength Field vs. Lab
Tensile Strength Field 200 psi
37Crack Development280 Cycles
38Actuator Force
39Crack Development2641 Cycles
37.5
17
40Surface SG Response
41Surface SG Response
42Surface SG Response
43Embedded SG Response
44Future Activities
- Experiment instrumentation
- Mill existing AC and overlay
- Full-scale test
- Laboratory tests
- Fracture energy of AC
- Creep compliance of AC
- Tensile strength of AC
- Thermal Coefficient of PCC
45Image Recording - North
46Image Recording - South