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Page 38
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
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Page 39
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 39
Page 40
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 40
Page 41
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 41
Page 42
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 42
Page 43
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 43
Page 44
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 44
Page 45
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 45
Page 46
Suggested Citation:"Appendix A - Dynamic Modulus Ruggedness Data." National Academies of Sciences, Engineering, and Medicine. 2008. Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press. doi: 10.17226/14200.
×
Page 46

Below is the uncorrected machine-read text of this chapter, intended to provide our own search engines and external engines with highly rich, chapter-representative searchable text of each book. Because it is UNCORRECTED material, please consider the following text as a useful but insufficient proxy for the authoritative book pages.

A1 A P P E N D I X A Dynamic Modulus Ruggedness Data

Friction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dynamic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformity Uniformity C min Air = 1 μmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FDM2-1 AAT 3 3 0 114 0 0 0 0 6.2 12181 9.8 3.6 5.5 9.3 0.1 FDM2-2 AAT 3 3 1 113 0 1 1 1 6.4 14509 11.4 9.8 9.9 11.8 .3 FDM2-3 AAT 3 5 0 77 0 0 1 1 6.1 14295 10.7 2.8 5.0 0.5 0.3 FDM2-4 AAT 3 5 1 72 0 1 0 0 6.0 17950 10.0 3.2 5.0 5.9 3.9 FDM2-5 AAT 5 3 0 69 0 1 0 1 5.9 17533 11.2 2.7 5.6 2.1 0.5 FDM2-6 AAT 5 3 1 72 0 0 1 0 6.1 13735 11.4 2.8 5.1 8.4 0.5 FDM2-7 AAT 5 5 0 101 0 1 1 0 5.8 14153 12.3 4.4 6.1 25.8 .0 FDM2-8 AAT 5 5 1 105 0 0 0 1 6.1 12609 11.4 2.9 4.6 14.5 .2 FDM3-1 AAT 3 3 0 97 0 0 0 0 5.7 17351 3.6 12.1 11.5 5.9 0.0 FDM3-2 AAT 3 3 1 104 0 1 1 1 5.6 16033 3.7 11.7 11.5 17.7 .6 FDM3-3 AAT 3 5 0 75 0 0 1 1 5.7 14755 3.9 4.6 5.5 3.0 0.4 FDM3-4 AAT 3 5 1 80 0 1 0 0 5.9 20579 4.6 7.4 9.6 6.4 0.7 FDM3-5 AAT 5 3 0 75 0 1 0 1 5.5 12477 5.2 5.7 6.6 14.6 .5 FDM3-6 AAT 5 3 1 75 0 0 1 0 5.7 14419 4.9 4.5 5.6 15.4 .1 FDM3-7 AAT 5 5 0 105 0 1 1 0 5.8 15840 5.6 13.3 13.0 55.3 .2 FDM3-8 AAT 5 5 1 121 0 0 0 1 5.7 13768 4.1 10.8 10.9 39.8 .2 FSM4-1 AAT 3 3 0 123 0 0 0 0 6.8 10214 7.3 3.4 4.8 9.4 5.2 FSM4-2 AAT 3 3 1 110 0 1 1 1 7.0 15451 8.5 11.2 10.6 11.4 .6 FSM4-3 AAT 3 5 0 75 0 0 1 1 6.7 14514 6.8 4.3 4.7 2.9 5.2 FSM4-4 AAT 3 5 1 80 0 1 0 0 6.8 13581 7.3 4.0 6.5 39.2 .8 FSM4-5 AAT 5 3 0 74 0 1 0 1 6.1 13221 8.8 4.3 5.1 14.0 .4 FSM4-6 AAT 5 3 1 74 0 0 1 0 5.8 12023 8.3 4.9 5.6 4.2 5.9 FSM4-7 AAT 5 5 0 122 0 1 1 0 6.3 12069 9.0 5.2 6.0 2.0 4.7 FSM4-8 AAT 5 5 1 121 0 0 0 1 6.5 13191 9.0 6.5 6.8 15.3 .5 FSM7-1 AAT 3 3 0 106 0 0 0 0 5.4 15500 6.5 13.4 12.9 19.0 0 1 0 0 1 0 0 2 6 3 5 5 5.2 FSM7-2 AAT 3 3 1 103 0 1 1 1 5.8 15779 7.2 12.7 12.9 2.1 5.9 FSM7-3 AAT 3 5 0 76 0 0 1 1 6.3 14226 7.0 4.9 6.1 2.6 5.4 FSM7-4 AAT 3 5 1 73 0 1 0 0 6.1 10878 7.0 5.0 6.5 0.7 5.8 FSM7-5 AAT 5 3 0 73 0 1 0 1 5.7 13400 10.6 4.5 6.0 8.0 7.4 FSM7-6 AAT 5 3 1 77 0 0 1 0 5.5 15092 8.4 4.4 6.0 1.0 5.5

Friction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dynamic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformity Uniformity C min Air = 1 μmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FSM7-7 AAT 5 5 0 121 0 1 1 0 5.4 13454 8.7 13.5 13.3 4.3 4.7 FSM7-8 AAT 5 5 1 117 0 0 0 1 5.8 13894 8.4 12.7 12.4 9.6 5.7 FDM4-1 FHWA 3 3 0 110 0 0 0 0 5.8 15668 12.2 4.3 4.0 11.8 .2 FDM4-2 FHWA 3 3 1 114 0 1 1 1 5.8 15101 13.9 3.5 3.9 21.2 .1 FDM4-3 FHWA 3 5 0 76 0 0 1 1 5.8 15507 11.9 3.2 3.2 24.4 .0 FDM4-4 FHWA 3 5 1 81 0 1 0 0 6.1 14761 14.5 2.7 4.4 12.6 .4 FDM4-5 FHWA 5 3 0 77 0 1 0 1 5.4 14035 14.4 3.2 4.3 11.2 .8 FDM4-6 FHWA 5 3 1 75 0 0 1 0 5.7 13469 14.2 3.4 3.4 10.3 .2 FDM4-7 FHWA 5 5 0 111 0 1 1 0 5.5 15482 15.8 4.4 4.3 23.9 .1 FDM4-8 FHWA 5 5 1 119 0 0 0 1 5.7 13347 13.7 2.1 4.7 22.2 .2 FDM5-1 FHWA 3 3 0 113 0 0 0 0 5.9 14749 11.9 3.2 3.4 17.6 .1 FDM5-2 FHWA 3 3 1 121 0 1 1 1 6.0 14294 14.6 2.9 3.4 12.3 .9 FDM5-3 FHWA 3 5 0 73 0 0 1 1 6.0 14510 12.1 5.1 4.7 18.5 .1 FDM5-4 FHWA 3 5 1 75 0 1 0 0 6.3 14473 14.0 4.6 4.7 22.3 .0 FDM5-5 FHWA 5 3 0 80 0 1 0 1 5.9 14673 15.5 3.5 4.1 4.4 3.6 FDM5-6 FHWA 5 3 1 76 0 0 1 0 5.9 13042 13.8 3.8 3.6 24.2 .6 FDM5-7 FHWA 5 5 0 124 0 1 1 0 6.3 13369 15.3 2.4 3.0 35.1 .1 FDM5-8 FHWA 5 5 1 124 0 0 0 1 6.2 13207 14.0 2.7 4.2 15.1 .4 FSM2-1 FHWA 3 3 0 121 0 0 0 0 6.7 13577 11.5 2.4 4.2 21.0 .1 FSM2-2 FHWA 3 3 1 126 0 1 1 1 6.5 12985 14.3 2.7 2.9 12.5 .7 FSM2-3 FHWA 3 5 0 77 0 0 1 1 6.2 14130 12.4 2.4 3.0 12.5 .2 FSM2-4 FHWA 3 5 1 76 0 1 0 0 6.5 13576 13.8 2.8 2.9 22.2 .4 FSM2-5 FHWA 5 3 0 75 0 1 0 1 6.5 11572 14.3 3.1 3.9 26.2 .4 FSM2-6 FHWA 5 3 1 78 0 0 1 0 6.5 10678 15.2 2.9 3.1 14.2 .5 FSM2-7 FHWA 5 5 0 127 0 1 1 0 6.4 11843 15.6 1.9 3.2 25.5 .6 FSM2-8 FHWA 5 5 1 126 0 0 0 1 6.0 13041 13.0 2.5 3.0 25.3 .2 FSM3-1 FHWA 3 3 0 124 0 0 0 0 6.1 13426 12.8 2.7 2.4 8.9 0.3 FSM3-2 FHWA 3 3 1 132 0 1 1 1 5.9 13191 16.8 3.8 4.0 12.4 .5 FSM3-3 FHWA 3 5 0 75 0 0 1 1 5.9 13981 12.7 3.1 3.5 5.5 0.8 FSM3-4 FHWA 3 5 1 77 0 1 0 0 5.5 14545 16.3 3.1 3.9 21.0 0 1 1 1 0 0 2 0 0 0 1 1 0 1 1 0 0 0 1 1 0 0 1 1 2.1

Friction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dynamic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformity Uniformity C min Air = 1 μmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FSM3-5 FHWA 5 3 0 86 0 1 0 1 6.6 13940 20.8 2.0 4.4 10.3 .0 FSM3-6 FHWA 5 3 1 76 0 0 1 0 6.4 13501 13.6 2.8 3.7 9.0 1.0 FSM3-7 FHWA 5 5 0 126 0 1 1 0 6.3 12187 16.4 1.8 3.2 12.6 .3 FSM3-8 FHWA 5 5 1 128 0 0 0 1 6.5 12399 14.6 1.7 2.5 6.9 0.5 FDM2-1 AAT 19 3 0 89 0 0 0 0 6.2 1266 35.4 0.8 8.5 22.9 .5 FDM2-2 AAT 19 3 1 114 0 1 1 1 6.4 1077 37.2 0.7 12.0 14.7 .8 FDM2-3 AAT 19 5 0 59 0 0 1 1 6.1 1204 37.4 2.0 6.6 15.8 .7 FDM2-4 AAT 19 5 1 55 0 1 0 0 6 1722 37.7 1.4 14.2 24.5 .1 FDM2-5 AAT 21 3 0 75 0 1 0 1 5.9 1246 37.9 1.0 7.9 25.4 .3 FDM2-6 AAT 21 3 1 64 0 0 1 0 6.1 1060 36.0 1.4 8.6 5.2 2.5 FDM2-7 AAT 21 5 0 83 0 1 1 0 5.8 1512 39.4 0.6 12.0 28.0 .9 FDM2-8 AAT 21 5 1 100 0 0 0 1 6.1 835 36.1 2.8 7.1 7.8 1.6 FDM3-1 AAT 19 3 0 99 0 0 0 0 5.7 1755 32.0 1.9 11.8 11.3 .9 FDM3-2 AAT 19 3 1 114 0 1 1 1 5.6 1645 31.2 0.5 11.8 0.1 6.4 FDM3-3 AAT 19 5 0 80 0 0 1 1 5.7 1264 33.4 2.1 6.1 6.7 6.9 FDM3-4 AAT 19 5 1 63 0 1 0 0 5.9 1601 35.4 1.9 12.3 19.2 .8 FDM3-5 AAT 21 3 0 89 0 1 0 1 5.5 1133 29.7 2.2 8.9 4.9 0.3 FDM3-6 AAT 21 3 1 86 0 0 1 0 5.7 1168 33.3 2.1 8.1 30.0 .8 FDM3-7 AAT 21 5 0 113 0 1 1 0 5.8 1457 31.5 0.8 10.5 15.1 .7 FDM3-8 AAT 21 5 1 109 0 0 0 1 5.7 1450 33.0 1.3 9.4 32.0 .1 FSM4-1 AAT 19 3 0 111 0 0 0 0 6.8 1292 27.7 0.6 6.0 12.7 .2 FSM4-2 AAT 19 3 1 126 0 1 1 1 7 1608 29.2 2.1 9.8 15.5 .3 FSM4-3 AAT 19 5 0 73 0 0 1 1 6.7 1613 27.3 0.9 4.6 11.5 .1 FSM4-4 AAT 19 5 1 77 0 1 0 0 6.8 1671 27.3 1.4 13.7 3.6 4.7 FSM4-5 AAT 21 3 0 88 0 1 0 1 6.1 1346 28.7 0.8 10.5 39.4 .9 FSM4-6 AAT 21 3 1 86 0 0 1 0 5.8 1382 26.5 1.0 4.0 61.4 .8 FSM4-7 AAT 21 5 0 109 0 1 1 0 6.3 1369 26.7 1.5 6.2 5.4 6.2 FSM4-8 AAT 21 5 1 113 0 0 0 1 6.5 1234 28.7 1.6 6.6 1.4 5.6 FSM7-1 AAT 19 3 0 101 0 0 0 0 5.4 2825 24.2 0.9 7.1 1.8 11.2 FSM7-2 AAT 19 3 1 111 0 1 1 1 5.8 1770 27.1 1.3 6.7 35.8 7 1 1 1 1 1 2 2 4 4 9 4 6 5 8 3 2 8 8.0

Friction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dynamic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformity Uniformity C min Air = 1 μmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FSM7-3 AAT 19 5 0 68 0 0 1 1 6.3 1737 26.8 0.9 5.8 8.3 6.3 FSM7-4 AAT 19 5 1 94 0 1 0 0 6.1 1259 27.7 0.8 6.1 5.7 3.9 FSM7-5 AAT 21 3 0 91 0 1 0 1 5.7 1295 28.1 0.8 4.4 18.4 .9 FSM7-6 AAT 21 3 1 70 0 0 1 0 5.5 1681 27.9 0.9 7.1 32.0 .2 FSM7-7 AAT 21 5 0 111 0 1 1 0 5.4 1429 27.8 0.6 7.2 51.4 .6 FSM7-8 AAT 21 5 1 110 0 0 0 1 5.8 1485 26.3 1.0 7.7 34.6 .8 FDM4-1 FHWA 19 3 0 109 0 0 0 0 5.8 1984 34.4 1.6 9.7 11.6 .5 FDM4-2 FHWA 19 3 1 107 0 1 1 1 5.8 1558 39.1 1.6 9.6 30.2 .4 FDM4-3 FHWA 19 5 0 67 0 0 1 1 5.8 1714 36.5 1.8 9.5 17.5 .7 FDM4-4 FHWA 19 5 1 69 0 1 0 0 6.1 1395 38.4 2.3 9.2 10.5 .1 FDM4-5 FHWA 21 3 0 64 0 1 0 1 5.4 1294 36.7 2.4 11.2 14.7 .1 FDM4-6 FHWA 21 3 1 67 0 0 1 0 5.7 1199 36.3 2.8 7.4 12.8 .6 FDM4-7 FHWA 21 5 0 105 0 1 1 0 5.5 1423 37.2 1.9 18.6 19.5 .8 FDM4-8 FHWA 21 5 1 106 0 0 0 1 5.7 1308 36.4 1.8 14.8 12.5 .8 FDM5-1 FHWA 19 3 0 107 0 0 0 0 5.9 1742 35.3 1.6 9.9 8.1 1.7 FDM5-2 FHWA 19 3 1 105 0 1 1 1 6 1476 35.9 1.5 6.8 8.4 0.4 FDM5-3 FHWA 19 5 0 66 0 0 1 1 6 1477 38.7 1.9 9.5 5.1 0.5 FDM5-4 FHWA 19 5 1 66 0 1 0 0 6.3 1392 39.8 2.6 10.5 14.1 .4 FDM5-5 FHWA 21 3 0 65 0 1 0 1 5.9 1216 42.2 3.0 10.2 4.0 1.6 FDM5-6 FHWA 21 3 1 64 0 0 1 0 5.9 1042 39.3 2.4 8.1 29.3 .3 FDM5-7 FHWA 21 5 0 101 0 1 1 0 6.3 1079 40.1 2.1 11.0 13.1 .3 FDM5-8 FHWA 21 5 1 108 0 0 0 1 6.2 1127 37.5 1.8 10.2 9.8 1.8 FSM2-1 FHWA 19 3 0 114 0 0 0 0 6.7 1820 30.0 2.7 7.9 10.1 .5 FSM2-2 FHWA 19 3 1 113 0 1 1 1 6.5 1628 33.4 2.6 9.7 5.6 0.5 FSM2-3 FHWA 19 5 0 72 0 0 1 1 6.2 1740 31.9 2.6 7.5 20.3 .4 FSM2-4 FHWA 19 5 1 69 0 1 0 0 6.5 1708 33.2 3.0 7.3 23.5 .5 FSM2-5 FHWA 21 3 0 67 0 1 0 1 6.5 1259 32.2 3.6 4.5 43.1 .0 FSM2-6 FHWA 21 3 1 72 0 0 1 0 6.5 1182 32.7 6.1 7.5 19.2 .6 FSM2-7 FHWA 21 5 0 113 0 1 1 0 6.4 1135 35.1 3.0 7.1 33.0 5 5 7 4 0 2 0 1 6 0 0 0 1 0 0 0 0 0 1 1 0.7 FSM2-8 FHWA 21 5 1 116 0 0 0 1 6 1628 31.5 3.0 8.1 3.9 0.3

Friction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dynamic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No = 0 Milled = 0 Teflon = 0 Voids Modulus Angle Se Se Uniformity Uniformity C min Air = 1 μmm/mm kPa Yes = 1 Sawed = 1 Latex = 1 % kPa Degree % % % % FSM3-1 FHWA 19 3 0 119 0 0 0 0 6.1 1760 30.4 1.8 7.0 23.3 .7 FSM3-2 FHWA 19 3 1 109 0 1 1 1 5.9 1835 28.4 1.7 7.7 18.1 .9 FSM3-3 FHWA 19 5 0 74 0 0 1 1 5.9 1758 30.8 2.2 5.4 14.2 .8 FSM3-4 FHWA 19 5 1 71 0 1 0 0 5.5 1636 32.9 2.6 6.6 13.4 .5 FSM3-5 FHWA 21 3 0 76 0 1 0 1 6.6 1297 35.9 3.5 6.6 11.1 .5 FSM3-6 FHWA 21 3 1 69 0 0 1 0 6.4 1426 31.6 3.1 6.5 13.1 .6 FSM3-7 FHWA 21 5 0 111 0 1 1 0 6.3 1654 36.7 1.8 7.8 22.8 .2 FSM3-8 FHWA 21 5 1 113 0 0 0 1 6.5 1146 33.5 2.5 6.4 7.5 1.8 FDM2-1 AAT 39 3 0 223 0 0 0 0 6.2 170 23.5 2.8 13.8 9.4 0.5 FDM2-2 AAT 39 3 1 288 0 1 1 1 6.4 131 23.0 3.2 14.8 4.3 0.3 FDM2-3 AAT 39 5 0 289 0 0 1 1 6.1 131 23.0 2.6 15.3 14.6 .2 FDM2-4 AAT 39 5 1 234 0 1 0 0 6 162 22.4 2.7 12.8 17.2 .3 FDM2-5 AAT 41 3 0 241 0 1 0 1 5.9 156 22.0 3.1 14.0 32.9 .1 FDM2-6 AAT 41 3 1 235 0 0 1 0 6.1 161 22.6 3.1 16.0 30.8 .1 FDM2-7 AAT 41 5 0 197 0 1 1 0 5.8 191 21.7 3.7 15.5 21.8 .1 FDM2-8 AAT 41 5 1 338 0 0 0 1 6.1 112 22.3 4.0 15.8 2.8 0.4 FDM3-1 AAT 39 3 0 119 0 0 0 0 5.7 164 30.4 3.2 32.6 15.9 .9 FDM3-2 AAT 39 3 1 176 0 1 1 1 5.6 111 34.5 3.7 34.0 82.3 .0 FDM3-3 AAT 39 5 0 92 0 0 1 1 5.7 121 13.3 4.2 26.1 43.4 .4 FDM3-4 AAT 39 5 1 81 0 1 0 0 5.9 138 14.6 4.7 40.7 22.4 17.6 FDM3-5 AAT 41 3 0 109 0 1 0 1 5.5 104 14.5 3.7 11.5 11.6 .2 FDM3-6 AAT 41 3 1 78 0 0 1 0 5.7 143 11.3 4.7 13.1 55.8 .7 FDM3-7 AAT 41 5 0 134 0 1 1 0 5.8 145 27.2 2.9 22.5 25.2 .4 FDM3-8 AAT 41 5 1 179 0 0 0 1 5.7 108 17.5 2.9 14.9 50.8 .6 FSM4-1 AAT 39 3 0 155 0 0 0 0 6.8 125 23.7 2.9 10.9 22.1 .6 FSM4-2 AAT 39 3 1 142 0 1 1 1 7 138 29.1 3.2 19.4 17.2 .1 FSM4-3 AAT 39 5 0 51 0 0 1 1 6.7 223 19.8 3.4 38.2 9.8 4.1 FSM4-4 AAT 39 5 1 81 0 1 0 0 6.8 140 20.1 4.8 45.6 22.6 0 3 0 0 4 1 4 1 1 0 0 1 3 6 7 8 8 5 9 7 6 4.9 FSM4-5 AAT 41 3 0 90 0 1 0 1 6.1 126 19.5 4.0 25.7 6.9 7.0 FSM4-6 AAT 41 3 1 66 0 0 1 0 5.8 172 16.8 5.3 11.6 1.8 6.9

F riction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dy namic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformit y Uniformity C min Air = 1 µmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FSM4-7 AAT 41 5 0 135 0 1 1 0 6.3 145 27. 3 2 .8 26.7 41.7 19. 1 FSM4-8 AAT 41 5 1 108 0 0 0 1 6.5 179 18. 0 2 .3 41.2 19. 5 .6 FSM7-1 AAT 39 3 0 8 7 0 0 0 0 5.4 221 25. 4 5 .7 11.0 28. 0 .5 FSM7-2 AAT 39 3 1 8 1 0 1 1 1 5.8 239 29. 5 5 .3 20.5 13. 3 .2 FSM7-3 AAT 39 5 0 7 4 0 0 1 1 6.3 155 21. 4 6 .8 15. 7 1 .4 0. 5 FSM7-4 AAT 39 5 1 6 2 0 1 0 0 6.1 179 25. 9 7 .6 21.3 18. 1 .4 FSM7-5 AAT 41 3 0 6 4 0 1 0 1 5.7 159 21. 3 6 .8 10.1 30. 7 .8 FSM7-6 AAT 41 3 1 5 8 0 0 1 0 5.5 198 22. 6 7 .2 13.6 80. 3 .9 FSM7-7 AAT 41 5 0 102 0 1 1 0 5.4 190 30. 6 2 .7 24. 1 3 .4 1. 2 FSM7-8 AAT 41 5 1 110 0 0 0 1 5.8 253 21. 9 2 .7 10. 2 0 .8 0. 4 FSM2-1 FHWA 39 3 0 127 0 0 0 0 6.7 181 26. 2 3 .6 6.6 14. 0 .8 FSM2-2 FHWA 39 3 1 133 0 1 1 1 6.5 146 33. 8 3 .4 8. 2 3 .5 1. 7 FSM2-3 FHWA 39 5 0 7 6 0 0 1 1 6.2 160 29. 8 3 .7 7.0 26. 0 .4 FSM2-4 FHWA 39 5 1 7 2 0 1 0 0 6.5 155 29. 6 4 .7 7.8 14. 7 .7 FSM2-5 FHWA 41 3 0 7 4 0 1 0 1 6.5 121 31. 9 7 .1 21.5 56. 4 .5 FSM2-6 FHWA 41 3 1 7 9 0 0 1 0 6. 5 9 7 30. 5 4 .8 6.7 24. 9 .3 FSM2-7 FHWA 41 5 0 158 0 1 1 0 6. 4 9 3 27. 5 4 .1 22.2 32. 5 .7 FSM2-8 FHWA 41 5 1 135 0 0 0 1 6 161 26. 1 3 .1 7.5 12.7 2. 3 FSM3-1 FHWA 39 3 0 136 0 0 0 0 6.1 179 28. 2 2 .7 8.5 20. 5 .9 FSM3-2 FHWA 39 3 1 165 0 1 1 1 5.9 161 34. 5 2 .4 10. 3 9 .8 5. 0 FSM3-3 FHWA 39 5 0 7 9 0 0 1 1 5.9 148 32. 8 3 .9 6.2 16. 9 .6 FSM3-4 FHWA 39 5 1 7 7 0 1 0 0 5.5 145 39. 1 4 .3 9.0 30. 9 .9 FSM3-5 FHWA 41 3 0 9 8 0 1 0 1 6. 6 7 7 38. 1 6 .3 15.8 16. 6 .2 FSM3-6 FHWA 41 3 1 133 0 0 1 0 6.4 159 25. 6 2 .7 7.7 11. 5 .6 FSM3-7 FHWA 41 5 0 154 0 1 1 0 6.3 100 29. 6 3 .6 14.6 34. 0 .8 FSM3-8 FHWA 41 5 1 144 0 0 0 1 6.5 114 26. 2 3 .4 8.5 15. 6 .8 FDM2-1 AAT 39 3 0 196 135 0 0 6.2 189 14. 0 2 .1 11.2 10. 7 .6 FDM2-2 AAT 39 3 1 128 145 1 1 6.4 409 9. 7 2 .5 6.4 12. 5 .0 FDM2-3 AAT 39 5 0 8 7 135 1 1 6.1 428 8. 8 1 .7 6. 3 0 .1 0. 8 FDM2-4 AAT 39 5 1 7 9 145 0 0 6 676 7. 0 2 .9 8.6 12. 6 5 1 1 1 0 2 0 2 0 2 3 3 1 2 5 2 0 0 1 2 0 1 .5

F riction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dy namic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformit y Uniformity C min Air = 1 µmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FDM2-5 AAT 41 3 0 136 145 0 1 5.9 474 8. 3 1 .7 7.9 40. 3 .0 FDM2-6 AAT 41 3 1 187 135 1 0 6.1 198 14. 5 1 .6 8.4 12. 8 .5 FDM2-7 AAT 41 5 0 214 145 1 0 5.8 173 13. 9 1 .7 11.7 17. 3 .8 FDM2-8 AAT 41 5 1 146 135 0 1 6.1 452 5. 5 1 .0 8. 3 7 .3 0. 1 FDM3-1 AAT 39 3 0 9 0 135 0 0 5.7 545 13. 5 1 .2 19. 4 0 .5 6. 2 FDM3-2 AAT 39 3 1 7 7 145 1 1 5.6 253 21. 9 2 .6 20.9 53. 3 .2 FDM3-3 AAT 39 5 0 8 4 135 1 1 5.7 442 12. 2 2 .2 12.6 35. 4 .2 FDM3-4 AAT 39 5 1 5 6 145 0 0 5.9 871 9. 6 1 .4 7.9 84.2 10. 6 FDM3-5 AAT 41 3 0 124 145 0 1 5.5 298 16. 3 1 .5 19.6 16. 7 .7 FDM3-6 AAT 41 3 1 7 6 135 1 0 5.7 648 8. 4 1 .8 10. 1 9 .3 6. 0 FDM3-7 AAT 41 5 0 3 5 145 1 0 5.8 560 26. 2 3 .1 51. 3 5 .4 6. 1 FDM3-8 AAT 41 5 1 9 2 135 0 1 5.7 213 17. 1 2 .8 10.9 48. 3 .7 FDM4-1 AAT 39 3 0 6 3 135 1 0 0 5.8 632 14. 6 2 .0 10. 6 8 .2 0. 7 FDM4-2 AAT 39 3 1 7 4 145 1 1 1 5.8 668 17. 5 1 .6 4. 7 4 .8 4. 3 FDM4-3 AAT 39 5 0 4 0 135 1 1 1 5.8 672 19. 4 2 .4 24. 5 6 .0 3. 6 FDM4-4 AAT 39 5 1 4 5 145 1 0 0 6.1 678 15. 3 1 .9 4. 3 5 .4 0. 3 FDM4-5 AAT 41 3 0 4 2 145 1 0 1 5.4 499 14.7 25.4 40. 4 3 .6 3. 4 FDM4-6 AAT 41 3 1 3 0 135 1 1 0 5.7 557 23. 1 3 .0 8.4 32. 3 .5 FDM4-7 AAT 41 5 0 8 6 145 1 1 0 5.5 589 15. 2 1 .9 11.0 14. 3 .0 FDM4-8 AAT 41 5 1 6 8 135 1 0 1 5.7 639 17. 1 1 .9 5.7 20. 5 .2 FDM5-1 AAT 39 3 0 9 8 135 1 0 0 5.9 598 12. 5 1 .6 24.2 19. 0 .2 FDM5-2 AAT 39 3 1 111 145 1 1 1 6 681 11. 0 1 .3 6.2 13. 0 .9 FDM5-3 AAT 39 5 0 6 3 135 1 1 1 6 630 13. 3 2 .0 9. 7 9 .0 2. 9 FDM5-4 AAT 39 5 1 4 9 145 1 0 0 6.3 680 14. 1 2 .3 17. 3 9 .4 0. 6 FDM5-5 AAT 41 3 0 4 7 145 1 0 1 5.9 490 17. 6 3 .0 19.3 11. 9 .1 FDM5-6 AAT 41 3 1 4 4 135 1 1 0 5.9 710 17. 4 2 .3 4.7 13. 2 .5 FDM5-7 AAT 41 5 0 7 5 145 1 1 0 6.3 628 13. 8 1 .6 12. 7 3 .3 2. 9 FDM5-8 AAT 41 5 1 7 5 135 1 0 1 6.2 620 15. 5 1 .4 15. 9 5 .2 1. 0 FSM2-1 FHWA 39 3 0 7 8 135 1 0 0 6.7 528 20. 0 2 .5 4. 4 6 .8 1. 3 FSM2-2 FHWA 39 3 1 127 145 1 1 1 6.5 339 24. 2 1 .7 6.2 12. 3 1 1 1 2 6 4 1 6 1 3 1 0 3 3 0 .6

F riction ID Lab Test Transfer Fluid Confining Membrane End Reducer Air Dy namic Phase Load Strain Strain Phase Temp Time Water = 0 Strain Pressure No =0 Milled =0 Teflon =0 Voids Modulus Angle Se Se Uniformit y Uniformity C min Air = 1 µmm/mm kPa Yes =1 Sawed =1 Latex =1 % kPa Degree % % % % FSM2-3 FHWA 39 5 0 4 3 135 1 1 1 6.2 517 21. 6 3 .0 31.5 15. 3 .6 FSM2-4 FHWA 39 5 1 9 6 145 1 0 0 6.5 267 25. 2 2 .9 5.4 23. 3 .4 FSM2-5 FHWA 41 3 0 4 5 145 1 0 1 6.5 575 19. 7 2 .6 14.9 31. 0 .1 FSM2-6 FHWA 41 3 1 6 2 135 1 1 0 6.5 235 26. 1 4 .4 7.9 17. 1 .4 FSM2-7 FHWA 41 5 0 7 3 145 1 1 0 6.4 480 18. 7 2 .2 17.3 37. 6 .4 FSM2-8 FHWA 41 5 1 118 135 1 0 1 6 254 25.4 2.1 5.9 13.1 1. 1 FSM3-1 FHWA 39 3 0 8 9 135 1 0 0 6.1 595 19. 4 1 .7 21.3 31. 3 .6 FSM3-2 FHWA 39 3 1 105 145 1 1 1 5.9 410 18. 8 1 .6 7.1 40. 9 .0 FSM3-3 FHWA 39 5 0 5 0 135 1 1 1 5.9 580 26. 1 2 .7 16.8 48. 8 .7 FSM3-4 FHWA 39 5 1 6 3 145 1 0 0 5.5 427 22. 1 2 .7 11.1 17. 9 .2 FSM3-5 FHWA 41 3 0 4 5 145 1 0 1 6.6 837 22. 5 2 .2 15. 5 5 .8 6. 7 FSM3-6 FHWA 41 3 1 6 3 135 1 1 0 6.4 368 26. 3 4 .3 5.7 26. 4 .8 FSM3-7 FHWA 41 5 0 9 4 145 1 1 0 6.3 650 15. 8 1 .8 24.2 19. 8 .4 FSM3-8 FHWA 41 5 1 150 135 1 0 1 6.5 173 34. 5 2 .3 16.6 62. 4 .1 FSM4-1 FHWA 39 3 0 119 135 1 0 0 6.8 310 18. 8 1 .8 8.8 24. 5 .5 FSM4-2 FHWA 39 3 1 143 145 1 1 1 7 259 18.9 1.8 7.4 22.4 6. 3 FSM4-3 FHWA 39 5 0 8 3 135 1 1 1 6.7 710 15. 7 1 .6 8.0 37. 7 .1 FSM4-4 FHWA 39 5 1 100 145 1 0 0 6.8 372 19. 7 2 .2 19.9 53. 5 .5 FSM4-5 FHWA 41 3 0 147 145 1 0 1 6.1 371 17. 8 2 .2 11.9 35. 6 .1 FSM4-6 FHWA 41 3 1 9 7 135 1 1 0 5.8 724 9. 6 2 .0 8.6 13. 6 .4 FSM4-7 FHWA 41 5 0 123 145 1 1 0 6.3 374 16. 5 2 .5 9.9 35. 2 .4 FSM4-8 FHWA 41 5 1 136 135 1 0 1 6.5 423 16. 0 2 .1 6.8 26. 5 .1 FSM7-1 FHWA 39 3 0 108 135 1 0 0 5.4 670 15. 8 1 .8 8.8 24. 5 .5 FSM7-2 FHWA 39 3 1 109 145 1 1 1 5.8 710 14. 4 1 .8 7.4 22. 4 .3 FSM7-3 FHWA 39 5 0 112 135 1 1 1 6.3 620 14. 6 1 .6 8.0 37. 7 .1 FSM7-4 FHWA 39 5 1 8 9 145 1 0 0 6.1 691 14. 4 2 .2 19.9 53. 5 .5 FSM7-5 FHWA 41 3 0 6 6 145 1 0 1 5.7 713 11. 6 2 .2 11.9 35. 6 .1 FSM7-6 FHWA 41 3 1 8 6 135 1 1 0 5.5 732 13. 4 2 .0 8.6 13. 6 .4 FSM7-7 FHWA 41 5 0 120 145 1 1 0 5.4 667 11. 5 2 .5 9.9 35. 2 .4 FSM7-8 FHWA 41 5 1 127 135 1 0 1 5.8 678 14. 0 2 .1 6.8 26. 5 1 0 3 1 4 4 6 7 3 4 1 8 5 3 6 5 5 7 2 5 6 3 6 5 5 7 2 .1

Next: Appendix B - Flow Number Ruggedness Data »
Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester Get This Book
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 Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester
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TRB’s National Cooperative Highway Research Program (NCHRP) Report 629: Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester examines ruggedness testing that was conducted with a simple performance tester for the dynamic modulus and flow number tests.

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