Full-scale Reflective Cracking Test Update - PowerPoint PPT Presentation

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Full-scale Reflective Cracking Test Update

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Full-scale Reflective Cracking Test Update Presented to: FAA Airport Pavement Working Group Meeting By: Hao Yin, Ph.D., P.E. Gemini Technologies, Inc. – PowerPoint PPT presentation

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Title: Full-scale Reflective Cracking Test Update


1
Full-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

2
Acknowledgement
  • 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

3
Objective
Generate information from full-scale tests
(NAPTF) to assist in the improvement of current
design procedures for AC overlay on rigid airport
pavements.
4
Scope
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
5
Key Parameters
1. Pavement Temperature T32oF, DT17oF
6
Key Parameters
2. Horizontal Displacement at Joint 15 mils
7
Key Parameters
3. Loading Rate ? 4. AC-PCC Interface Bond ?
8
Progress Since 2011
  • Laboratory tests
  • Construction, instrumentation, and data
    collection
  • Temperature Effect Simulation System (TESS)
    tune-up and enhancements
  • Trial test

9
Texas Overlay Tester
Determination of Loading Rate
Temp 32 oF Max Hori Dip 15 mils Loading Rate
0.25, 0.50, 1.0 mil/sec
10
Overlay Tester Results
11
Interface Bond Experiment
12
Bond Strength Test
Temp 32 oF Loading Rate 0.05 mil/sec
13
Bond Strength Test
14
Bond Strength Test
15
Temperature Unit Re-design
16
Pavement Construction
17
Pavement Construction
18
Pavement Construction
19
Pavement Construction
20
Instrumentation 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
21
Data 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
26
Crack Arrester
27
Trial 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

28
Hydraulic Control
29
Hydraulic Control Cont.
30
Hori Dis Along Joint
North
South
31
Pavement Temperature
32
Crack Development36 Cycles
33
Crack Development180 Cycles
34
Crack initiation
35
Dynamic Modulus
36
Tensile Strength Field vs. Lab
Tensile Strength Field 200 psi
37
Crack Development280 Cycles
38
Actuator Force
39
Crack Development2641 Cycles
37.5
17
40
Surface SG Response
41
Surface SG Response
42
Surface SG Response
43
Embedded SG Response
44
Future 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

45
Image Recording - North
46
Image Recording - South
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