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February 1, 20 05 1 Analysis of Test Slab Failure Data Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic City, NJ Airport Pavement Working Group Meeting Sheraton Atlantic City Convention Center Hotel

February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

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Page 1: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 1

Analysis of Test Slab Failure DataAnalysis of Test Slab Failure Data

David R. BrillFAA Airport Technology R&D Branch, AAR-410

William J. Hughes Technical Center, Atlantic City, NJAirport Pavement Working Group Meeting

Sheraton Atlantic City Convention Center HotelFebruary 2, 2005

Page 2: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 2 AAR-410

ObjectivesObjectives

Quantify CC2 rigid test item performance and failure using the SCI concept.

Relate to historical rigid full-scale tests (Lockbourne, Sharonville, MWHGL etc.).

Compare with current failure model. Analyze effects of test variables:

Support type (stabilized base vs. conventional). 4-wheel vs. 6-wheel. Traffic on outside lane.

Page 3: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 3 AAR-410

CC2 Test Item LayoutCC2 Test Item Layout

C EN TER LIN E

22.9 m (75 ft)

18.3

m (

60 f

t)

22 .9 m (75 ft)22.9 m (75 ft)

M R C M R G M R SN orth C arriageTrafficked A rea

South C arriageTrafficked A rea

D irection ofTraffic

7.6 m (25 ft) T ransitionArea (Typ.)

Page 4: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

Construction Cycle 2 – Trafficking MRCConstruction Cycle 2 – Trafficking MRC

MRC trafficking

stopped on June 24,

2004 (north side after

12,675 passes and

south side after 5,402

passes.

A total of 96 cracks

were detected and 20

cores taken.

400'

325'

C19

C20

C18

C17

C14

C16

C15

CS

C12

C11

C6

C10C9

CSC8

CS

5

15

24

25

23

CS CS

S12 S17

S11

1

2

17

22

26

27

S7S2

S1 S6

29

32

33

S16

CS

CS CS

S9

S3 S8

S5

S4

S10

30

31

34

CSCS

CS

CS

CS

CS

S20S15

6

16

CS CS

S14 S19

14

13

28

CS

CS

S13 S18

3

4

10

7

9

12

11

8

19

21

20

35

36

37

38

39

C1

C2

C3

C4

C5

C7

40

41

42

43

44

4645

48

47

49

50

51

52

18

54

53

5655

57

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5960

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71 72

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C13

75

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77

CS

CS

CS

78

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81

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83

86 85

84

87

88

89

90

9192

93

94

96

95

North South

Page 5: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 5 AAR-410

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3

2

17

8

9

10

11

12

13

15

16

17

18

22

21

23

19

26

25

27

28

29

3031

33

32

34

35

36

37

38

40

41

48

42

43

44

45

47

49

50

51

53

54

55

56

58

59

61

6263

64

66

67

68

69

70

71

72

75

73

74

76

78

81

80

82

84

85

86

87

88

89

90

9192

9394

95

9697

98

99

100

102

10

103

108

106

105

107

104

109

112113

114

115

121

11

120 122

123

118

124

126

127128

129125

130

131

132

133

134

135

136

137

138

139

140

141

142

143

145

117 146

147

148

151

152

153

154

77

155

158

157156

159 160

161

162

163

164

165

166

168

169

167

170

171

172

175

174

176

173

177

178

182

181

14 180

179 184

183

185

52

79

186

187

65188

189

191

190

20

192

193

194

195 196

111

144

116

60 197

24

201

202

199

198

201

39

203

83

204

205

206

149

150

207

208

46

110

57

210209

211

500'

425'

S32 S37S27S22

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

S32 S37

S31

S27S22

S21 S26 S36

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

6

5

4

3

2

1

7

8

9

10

11

12

13

15

16

17

18

22

21

23

19

26

25

27

28

29

3031

33

32

34

35

36

37

38

40

41

42

43

44

45

49

50

51

53

54

56

58

61

62

63

64

66

67

68

69

70

71

72

75

73

74

76

78

81

80

84

86

87

88

89

90

9192

93

94

95

9697

98

99

100

102

10

103

108

106

107

113

114

115

121

11

120 122

123

118126

127128

129125

130

131

132

133

134

136

137

138

140

141

142

143

145

117146

147

148

151

152

153

154

77

155

158

157156

159

161

162

163

164

165

166

168

169

167

170

171

172

175

174

176

173

177

178

182

181

14 180

179 184

183

185

52

79

186

187

65

188

189

191

190

20

192

193

194

195

196

111

144

116

60 197201

202

199

198

201

39

203

83

204

205

206

149

150

207

208

46

110

57

209

212

124214

213

215

216

217

218

219

135

220

104

105

85221

82

222

139

223224

225

160109

55

112

210

47

228

227

226

229

59 48

230

211

24

231

232

500'

425'

S32 S37S27S22

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

S32 S37

S31

S27S22

S21 S26 S36

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

6

5

4

3

2

1

7

8

9

10

11

12

13

15

16

17

18

22

23

19

26

25

27

28

29

3031

33

32

34

35

38

40

41

42

43

44

45

49

50

51

53

54

56

61

62

63

64

66

67

68

69

70

71

72

75

74

76

78

81

80

86

87

88

89

91

9293

94

95

9697

98

99

100

102

10

103

108

106

107

113

114

115

121

11

120 122

123

118126

127128

129125

130

131

132

133

136

137

138

140

141

142

143

145

117146

147

148

151

152

153

154

77

155

158

157156

159 161

162

163

164

165

166

168

170

172

175

174

176

173

177

178

182

181

14180

179184

183

185

52

79

186

187

65

188

189

191

190

20

192

193

194

196

111

144

116

60 197201

202

199

198

201

39

203

83

204205

206

149

150

207

208

46

110

57

209

212

124214

213

215

216

217

218

219

135

220

104

105

85221

82

222

139

223224

225

160109

55

112

210

47

228

227

226

229

59 48

230

211

24

232

21

84

233

234134

167

16990

235

237195

36238

73

37

239

240

58

236

171

241

231

242

500'

425'

S32 S37S27S22

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

S32 S37

S31

S27S22

S21 S26 S36

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

6

5

4

3

2

1

7

8

9

10

11

12

13

15

16

17

18

22

23

19

26

25

27

28

29

30

31

33

32

34

35

38

40

41

42

43

44

45

49

50

51

53

54

56

61

62

63

64

66

67

68

69

70

71

72

75

74

76

78

81

80

86

87

88

89

91

9293

94

95

9697

98

99

100

102

10

103

108

106

107

113

114

115

121

11

120 122

123

118126

127128

129125

130

131

132

133

136

137

138

140

141

142

143

145

117146

147

148

151

152

153

154

77

155

158

157156

159 161

162

163

164

165

166

168

170

172

175

174

176

173

177

178

182

181

14180

179184

183

185

52

79

186

187

65

188

189

191

190

20

192

193

194

196

111

144

116

60 197201

202

199

198

201

39

203

83

204205

206

149

150

207

208

46

110

57

209

212

124214

213

215

216

217

218

219

135

220

104

105

85221

82

222

139

223224

225

160109

55

112

210

47

228

227

226

229

59 48

230

211

24

232

21

84

233

234134

167

16990

235

237195

36238

73

37

239 240

58

236

241

231

242

171243

244

Construction Cycle 2:Construction Cycle 2:Trafficking Test Item MRGTrafficking Test Item MRG

MRG After

31,020 Passes

7/13/2004 7/14/2004 7/19/2004 7/20/2004 7/27/2004

Spall 8/2/2004 8/9/2004

8/11/2004 8/16/2004 8/18/2004 8/20/2004 8/24/2004 8/26/2004 8/27/2004 8/31/2004 9/7/2004 9/9/2004

9/14/2004 9/21/2004 9/28/2004 10/5/2004

10/13/2004 10/29/2004 11/9/2004

11/16/2004 11/23/2004 12/02/2004 12/07/2004 12/14/2004

Page 6: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 6 AAR-410

500'

425'

S32 S37S27S22

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

S32 S37

S31

S27S22

S21 S26 S36

S29

S23 S28

S25

S24

S30 S40S35

S34 S39

S33 S38

6

5

4

3

2

1

7

8

9

10

11

12

13

15

16

17

18

22

23

19

26

25

27

28

29

30

31

33

32

34

35

38

40

41

42

43

44

45

49

50

51

53

54

56

61

62

63

64

66

67

68

69

70

71

72

75

74

76

78

81

80

86

87

88

89

91

9293

94

95

9697

98

99

100

102

10

103

108

106

107

113

114

115

121

11

120 122

123

118126

127128

129125

130

131

132

133

136

137

138

140

141

142

143

145

117146

147

148

151

152

153

154

77

155

158

157156

159 161

162

163

164

165

166

168

170

172

175

174

176

173

177

178

182

181

14180

179184

183

185

52

79

186

187

65

188

189

191

190

20

192

193

194

196

111

144

116

60 197201

202

199

198

201

39

203

83

204205

206

149

150

207

208

46

110

57

209

212

124214

213

215

216

217

218

219

135

220

104

105

85221

82

222

139

223224

225

160109

55

112

210

47

228

227

226

229

59 48

230

211

24

232

21

84

233

234134

167

16990

235

237195

36238

73

37

239 240

58

236

241

231

242

171243

244

MRG After

31,020 Passes

7/13/2004 7/14/2004 7/19/2004 7/20/2004 7/27/2004

Spall 8/2/2004 8/9/2004

8/11/2004 8/16/2004 8/18/2004 8/20/2004 8/24/2004 8/26/2004 8/27/2004 8/31/2004 9/7/2004 9/9/2004

9/14/2004 9/21/2004 9/28/2004 10/5/2004

10/13/2004 10/29/2004 11/9/2004

11/16/2004 11/23/2004 12/02/2004 12/07/2004 12/14/2004

Page 7: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 7 AAR-410

600'

525'

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1600'

525'

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

600'

525'

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

600'

525'

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

16

17

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

2324

25

26

27

28

29

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

2324

25

26

27

28

29

30

32

31

600'

525'

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

89

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

2324

25

26

27

28

29

30

32

3135

34

33

600'

525'

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

2324

25

26

27

28

29

30

32

3135

34

33

36

37

38 39

40

41

42

43

44

45

46

600'

525'

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19

20

21

22

2324

25

26

27

28

29

30

32

3135

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

4748

C5

5152

50

53

600'

525'

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

CS

10

11

12

13

14

15

16

17

18

19 20

21

22

2324

25

26

27

28

29

30

32

3135

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

4748

5152

50

53

54

55

56

57

58

59

60

61 600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

1920

21

22

2324

25

26

27

28

29

30

32

3135

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

4748

5152

50

53

54

55

56

57

58

59

60

6163

62600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

1920

21

22

2324

25

26

27

28

29

30

32

35

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

4748

5152

50

53

54

55

56

57

58

59

60

616362

64

65

31

68

6766

69

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

19 20

21

22

2324

25

26

27

28

29

30

32

35

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

47

48

5152

50

53

54

55

56

57

58

59

60

616362

64

65

31

68

6766

69

72

71

70

7374

75

76

77

78

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

19 20

21

22

2324

25

26

27

28

29

30

32

35

34

33

36

37

38 39

40

41

42

43

44

45

46

C3

49

47

48

5152

50

53

54

55

56

57

58

59

60

616362

64

65

31

68

6766

69

72

71

70

7374

75

76

77

78

8079

81 82

8384

85

86

87

88

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

20

21

22

2324

25

26

27

28

29

30

32

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C3

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616362

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7170

73 74

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4796

97

10098 99

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10

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104

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

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616362

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8384

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10098 99

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1063

10

111

110

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108

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

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1063

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116117

118119

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600'

525'

CS C5

C4

CS

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C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

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S54 S59

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102117

118119

120

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123124

125

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127

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128

600'

525'

CS C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

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19

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1063

10

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107

108

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102117

118119

120

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123124

125

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600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

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CS

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616362

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73 74

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8079

81 82

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19

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97

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116

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104

105

1063

10

111

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108

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115

102117

118119

121

122

120

123124

125

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131

132

133

135

134136

138137

139

600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

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CS

CS

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6766

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72

7170

73 74

75

7677

78

8079

81 82

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85

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55

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19

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59

4796

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104

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1063

10

1113

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107

108

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102117

118119

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134136

138

139

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115

142

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600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

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CS

CS

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616362

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6766

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72

7170

73 74

75

7677

78

8079

81 82

83

84

85

86

87

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89

55

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92

93

94

19

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59

4796

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10098

99

101

116

103

104

105

1063

10

1113

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108

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118119

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123124

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134136

138

139

140

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115

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600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

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CS

CS

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46

C3

49

48

5152

50

53

54

56

57

58

60

616362

64

65

31

68

6766

69

72

7170

73 74

75

7677

78

8079

81 82

83

84

85

86

87

88

89

55

90

91

92

93

94

19

95

59

4796

97

10098

99

101116

103

104

105

1063

10

1113

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107

108

112

113

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102117

118119

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123124

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134136

138 139

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152

154

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CS

151

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600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

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CS

CS

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46

C3

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616362

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31

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6766

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72

7170

73 74

75

7677

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8079

81 82

83

84

85

86

87

88

89

55

90

91

92

93

94

19

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59

4796

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10098

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101116

103

104

105

1063

10

1113

110

107

108

112

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114

102117

118119

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123124

125

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134136

138

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152

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CS

151

153

155

156

128

600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

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CS

CS

10

11

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2324

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44 45

46

C3

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48

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50

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616362

64

65

31

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6766

69

72

7170

73 74

75

7677

78

8079

81 82

83

84

85

86

87

88

89

55

90

91

92

93

94

19

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59

4796

97

10098

99

101116

103

104

105

1063

10

1113

110

107

108

112

113

114

102117

118119

121

122

120

123124

125

126

127

129

130

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133

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134136

138

139

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128

7/13/2004 7/14/2004 7/16/2004 7/19/2004 7/20/2004

Corner Spall 7/21/2004

Core 8/2/2004 8/5/2004 8/9/2004

8/11/2004 8/12/2004 8/16/2004 8/18/2004 8/20/2004 8/24/2004 8/26/2004 8/27/2004 8/31/2004 9/7/2004 9/9/2004

9/14/2004 9/21/2004 9/28/2004 10/5/2004

10/13/2004 10/29/2004 11/9/2004

11/16/2004 11/23/2004 12/02/2004 12/07/2004 12/14/2004

CS

MRS After

30,996 Passes

Construction Cycle 2:Construction Cycle 2:Trafficking Test Item MRSTrafficking Test Item MRS

Page 8: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 8 AAR-410

600'

525'

CS

C5

C4

CS

C2

C1

S52 S57

S51

S47S42

S41 S46 S56

S49

S43 S48

S45

S44

S50 S60S55

S54 S59

S53 S58

1

4

2

3

5

6

7

8

9

CS

CS

CS

10

11

12

13

14

15

16

17

18

20

21

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2324

25

26

27

28

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30

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35

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41

42

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44 45

46

C3

49

48

5152

50

53

54

56

57

58

60

616362

64

65

31

68

6766

69

72

7170

73 74

75

7677

78

8079

81 82

83

84

85

86

87

88

89

55

90

91

92

93

94

19

95

59

4796

97

10098

99

101116

103

104

105

1063

10

1113

110

107

108

112

113

114

102117

118119

121

122

120

123124

125

126

127

129

130

131

132

133

135

134136

138

139

140

141

115

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150

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CS

151

153

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128

MRS After

30,996 Passes

7/13/2004 7/14/2004 7/16/2004 7/19/2004 7/20/2004

Corner Spall 7/21/2004

Core 8/2/2004 8/5/2004 8/9/2004

8/11/2004 8/12/2004 8/16/2004 8/18/2004 8/20/2004 8/24/2004 8/26/2004 8/27/2004 8/31/2004 9/7/2004 9/9/2004

9/14/2004 9/21/2004 9/28/2004 10/5/2004

10/13/2004 10/29/2004 11/9/2004

11/16/2004 11/23/2004 12/02/2004 12/07/2004 12/14/2004

CS

Page 9: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 9 AAR-410

CC2 Test Items - ResultsCC2 Test Items - Results Full-scale traffic testing began on 4/27/04. Trafficking ended 12/10/04. Passes completed:

Top-down cracking has not been eliminated, but bottom-up longitudinal cracks have occurred in the lane receiving loading from both lines of tires.

Passes CompletedTest Item Gear Type Apr-Jun 2004 Jul-Sep 2004 Oct-Dec 2004 TotalMRC - North 4-wheel 12675 0 0 12675MRC - South 4-wheel 5405 0 0 5405MRG - North 6-wheel 0 21186 9834 31020MRG - South 4-wheel 0 21162 9834 30996MRS - North 6-wheel 0 20262 0 20262MRS - South 4-wheel 0 21162 9834 30996

Page 10: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 10 AAR-410

Performance MonitoringPerformance Monitoring Visual Distress Surveys.

ASTM D 5340-93 and FAA AC 150/5380-6. Daily up to 10,000 passes. Weekly after 10,000 passes.

Embedded Sensors. Responses monitored for early indication of cracking.

Nondestructive Tests. HWD every 15 wanders (990 passes) up to 10,000

passes. Every 30 wanders after 10,000 passes. Destructive Testing.

Cores to investigate origin of cracks.

Page 11: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 11 AAR-410

Structural Condition Index (SCI)Structural Condition Index (SCI)

Rollings (1988) SCI is structural component of rigid PCI.

Only load related distress types are considered (e.g., L/T/D cracks, corner breaks, shattered slab).

SCI is always equal to or higher than PCI for the same pavement feature.

Joint and corner spalling was excluded from the SCI computation for CC2 test items.

Page 12: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 12 AAR-410

Micro PAVER ComputationsMicro PAVER Computations

Record structural distresses based on visual surveys.

Treat each test item (north side or south side) as a sample unit.

Follow ASTM procedures for counting distresses and assigning severity levels.

Page 13: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 13 AAR-410

CC2 Test Item DistressesCC2 Test Item DistressesMRS North - Shattered Slab MRG North - Corner Spall

MRG South - Longitudinal Crack Intersecting Corner BreakMRS North - Long. & Diag. Cracks

Page 14: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 14 AAR-410

SCI Versus Coverage AnalysisSCI Versus Coverage Analysis

Plot SCI as a function of applied coverages. P/C ratio is computed from wander pattern. All slabs in sample unit versus inside traffic lane only.

Obtain linear regression of SCI versus log(C). Intercept with SCI=100 line yields CO (cov. to 1st crack).

Intercept with SCI=0 line yields CF (cov. to full failure).

New rigid design concerned with coverages to SCI=80. Lower portions of failure curve (below SCI = 80) are

important for overlay designs.

Page 15: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 15 AAR-410

y = -60.606Ln(x) + 503.04

R2 = 0.9049

y = -29.763Ln(x) + 235.22

R2 = 0.8104

0

20

40

60

80

100

120

1 10 100 1000 10000

Coverages

SC

I

Current Failure Model (No Compensation) Current Failure Model (SB Compensation)

MRC-North (P/C = 3.80) MRC-South (P/C = 4.71)

Log. (MRC-North (P/C = 3.80)) Log. (MRC-South (P/C = 4.71))

PRELIMINARY DATAPRELIMINARY DATA

Test Item MRC - SCI versus Coverages Test Item MRC - SCI versus Coverages (All Distresses)(All Distresses)

Page 16: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 16 AAR-410

y = -72.715Ln(x) + 572.15

R2 = 0.821

y = -64.43Ln(x) + 506.04

R2 = 0.8269

0

20

40

60

80

100

120

1 10 100 1000 10000

Coverages

SC

I

Current Failure Model (No Compensation) Current Failure Model (SB Compensation)

MRC-North (P/C = 3.80) MRC-South (P/C = 4.71)

Log. (MRC-North (P/C = 3.80)) Log. (MRC-South (P/C = 4.71))

Test Item MRC - SCI versus Coverages Test Item MRC - SCI versus Coverages (Center Traffic Lane Distresses Only)(Center Traffic Lane Distresses Only)

PRELIMINARY DATAPRELIMINARY DATA

Page 17: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 17 AAR-410

y = -44.174Ln(x) + 374.94

R2 = 0.8957

y = -100.61Ln(x) + 871.57

R2 = 0.9611

0

20

40

60

80

100

120

1 10 100 1000 10000 100000 1000000

Coverages

SC

I

MRS-North (6 wheel, P/C = 4.71) MRS-South (4 wheel, P/C = 4.71)

Rigid Failure Model - 6 wheel (No Compensation) Rigid Failure Model - 4 wheel (No Compensation)

Rigid Failure Model - 6 wheel (SB compensation) Rigid Failure Model - 4 wheel (SB Compensation)

Log. (MRS-North (6 wheel, P/C = 4.71)) Log. (MRS-South (4 wheel, P/C = 4.71))

Test Item MRS - SCI versus CoverageTest Item MRS - SCI versus Coverage(Center Traffic Lane Distresses Only)(Center Traffic Lane Distresses Only)

PRELIMINARY DATAPRELIMINARY DATA

Page 18: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 18 AAR-410

0

20

40

60

80

100

120

1 10 100 1000 10000

Coverages

SC

I

MRG-North (6 wheel, P/C = 4.71) MRG-South (4 wheel, P/C = 4.71)

Rigid Failure Model - 6 wheel (no compensation) Rigid Failure Model - 4 wheel (no compensation)

Rigid Failure Model - 6 wheel (SB Compensation) Rigid Failure Model - 4 wheel (SB Compensation)

Log. (MRG-North (6-wheel, P/C = 4.71)) Log. (MRG-South (4-wheel, P/C = 4.71))

Test Item MRG - SCI versus CoverageTest Item MRG - SCI versus Coverage(Center Traffic Lane Distresses Only)(Center Traffic Lane Distresses Only)

PRELIMINARY DATAPRELIMINARY DATA

SCI = -246.96 log(C) + 935.11R2 = 0.9647

SCI = -247.03 log(C) + 941.57R2 = 0.9636

Page 19: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 19 AAR-410

CC2 Test Strip - SCI versus CoverageCC2 Test Strip - SCI versus Coverage(S Slab Distresses Only)(S Slab Distresses Only)

y = -39.228Ln(x) + 296.37

R2 = 0.9039

0

20

40

60

80

100

120

1 10 100 1000 10000

Coverages

SC

I

Test Strip: All 15-ft S Slabs (P/C = 4.13) Rigid Failure Model - S Slabs

Rigid Failure Model - S Slabs (SB Compensation) Log. (Test Strip: All 15-ft S Slabs (P/C = 4.13) )

S1

S2

S3

S4

C1

S5

S6

C3

C2

C5

C6

C4

4

14

24

36

12

48

18

3

19

20

43

47

39

16

21

52

25

50

26

55

27

35

46

28

56

57

29

51

32

38

60

22

15

6

45

44

37

37

49

17

58

33

41

53

40

3159

30

54

42

11

1

21

23

1

6

8

3

7

8

54

7

1029

5

13

34

S SLABSC SLABS

PRELIMINARY DATAPRELIMINARY DATA

Page 20: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 20 AAR-410

Summary of SCI vs. CoverageSummary of SCI vs. Coverage

0

20

40

60

80

100

100 1000 10000

Coverages

SC

I

MRC-North MRC-South MRS-North MRS-South

MRG-North MRG-South CC2 Test Strip

CC2 Test Strip

MRC-South

MRC-North

MRS-North

MRG-North

MRG-South

MRS-South

Page 21: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 21 AAR-410

Regression Data for SCI vs. Regression Data for SCI vs. Log of Coverages Log of Coverages (preliminary)(preliminary)

R e g r e s s i o n C o n s t a n t s 1

T e s t I t e m A B R 2C o v e r a g e s t oI n i t i a l C r a c k , C O

C o v e r a g e s t oF u l l F a i l u r e , C F

P / C

M R C - N - 1 6 7 . 4 3 5 7 2 . 1 5 0 . 8 2 1 6 6 1 2 6 1 3 3 . 8 0M R C - S - 1 4 8 . 3 6 5 0 6 . 0 4 0 . 8 2 7 5 4 6 2 5 7 6 4 . 7 1M R G - N - 2 4 7 . 0 3 9 4 1 . 5 7 0 . 9 6 4 2 5 5 1 6 4 8 0 4 . 7 1M R G - S - 2 4 6 . 9 6 9 3 5 . 1 2 0 . 9 6 5 2 4 0 8 6 1 1 7 4 . 7 1M R S - N - 1 0 1 . 7 1 3 7 4 . 9 4 0 . 8 9 6 5 0 5 4 8 5 5 4 . 7 1M R S - S - 2 3 1 . 6 6 8 7 1 . 5 7 0 . 9 6 1 2 1 4 1 5 7 8 4 4 . 7 1T e s t S t r i p - 9 0 . 3 3 2 9 6 . 3 7 0 . 9 0 4 1 4 9 1 9 1 0 4 . 1 31 BCA logSCI

Page 22: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 22 AAR-410

Design Factor vs. CoveragesDesign Factor vs. Coverages

Design Factor (DF) = ratio of concrete flexural strength to maximum calculated bending stress.

LEDFAA model based on Rollings (1988) regression: DF = 0.5234 + 0.3920 log (CO) coverages to onset of cracking

DF = 0.2967 + 0.3881 log (CF) coverages to full failure (SCI 0)

Recompute design factors for all test items using FEDFAA (3D-FEM) edge stress.

Evaluate parameters including 7 new NAPTF data points. Preliminary analysis - design factors subject to change as

we continue to characterize the material properties.

Page 23: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 23 AAR-410

Recalculate Design FactorsRecalculate Design Factors(Historic Full-Scale Test Data)(Historic Full-Scale Test Data)

0

0.5

1

1.5

2

2.5

1 10 100 1000 10000 100000

Coverages to Complete Failure, CF

DF

Rollings Model MWHGL KLJS

SSPS Lockbourne 1 Lockbourne 2

Sharonville New Data Regression

Original Regression

Recalculated Using FEDFAA Edge Stress

Page 24: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 24 AAR-410

Design Factor vs. Coverages Design Factor vs. Coverages (Coverages to Complete Failure, SCI=0)(Coverages to Complete Failure, SCI=0)

0

0.5

1

1.5

2

2.5

1 10 100 1000 10000 100000

Coverages to Complete Failure, CF

DF

Rollings Model NAPTF MWHGLKLJS SSPS Lockbourne 1Lockbourne 2 Sharonville New Data Regression

MRC-NORTH

MRC-SOUTHTEST STRIP - S

MRS-NORTH

MRS-SOUTH

MRG-SOUTH

MRG-NORTH

PRELIMINARY DATAPRELIMINARY DATA

Page 25: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 25 AAR-410

0

0.5

1

1.5

2

2.5

1 10 100 1000 10000

Coverages to Onset of Deterioration, C0

DF

Rollings Model NAPTF MWHGL

KLJS SSPS Lockbourne 1

Lockbourne 2 Sharonville New Regression (Type I and IIA Only)

MRC-NORTH

MRC-SOUTH

TEST STRIP - S

MRS-NORTH

MRS-SOUTH MRG-NORTH

MRG-SOUTH

Design Factor vs. Coverages Design Factor vs. Coverages (Coverages to Onset of Failure, SCI=100 (Coverages to Onset of Failure, SCI=100 --))

PRELIMINARY DATAPRELIMINARY DATA

Page 26: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 26 AAR-410

Current EffortsCurrent Efforts

Finalize material characterization (e.g., concrete strength, subgrade properties) for design factor computation.

Finalize “best fit” parameters for FAARFIELD rigid failure model from full-scale test data.

Re-evaluate current base stiffness compensation model considering: full-scale test results showing straight-line trend. improved ability of 3D-FEM model to give accurate

stresses for stabilized base structures.

Page 27: February 1, 20051 Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic

February 1, 2005 27 AAR-410

Questions?Questions?