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Page 47
Suggested Citation:"Appendix B - Flow Number 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 47
Page 48
Suggested Citation:"Appendix B - Flow Number 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 48
Page 49
Suggested Citation:"Appendix B - Flow Number 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 49
Page 50
Suggested Citation:"Appendix B - Flow Number 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 50
Page 51
Suggested Citation:"Appendix B - Flow Number 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 51

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B1 A P P E N D I X B Flow Number Ruggedness Data

Friction ID Lab Temp Transfer Fluid End Reducer Confining Deviator Contact Dwell Air Flow Permanent Strain, % C Time 0=Water 0=Milled 0=Teflon Stress Stress Stress Time Void # 500 1000 2000 5000 8000 Min 1=Air 1=Sawed 1=Latex kPa kPa kPa sec % Cycles Cycles Cycles Cycles Cycles Cycles FDM10-1 FHWA 49 3 0 0 0 0 144 5 0.95 6.5 1401 1.1 1.3 1.8 FDM10-2 FHWA 49 3 1 1 1 0 144 5 0.85 6.4 1601 0.9 1.1 1.6 FDM10-3 FHWA 49 5 0 1 1 0 135 5 0.95 6.4 1241 0.9 1.2 1.7 FDM10-4 FHWA 49 5 1 0 0 0 134 5 0.85 6.3 1341 1.1 1.4 1.9 FDM10-5 FHWA 51 3 0 0 1 0 135 5 0.85 6.3 641 1.2 1.6 2.7 FDM10-6 FHWA 51 3 1 1 0 0 134 5 0.95 6.3 1001 1.1 1.5 2.5 FDM10-7 FHWA 51 5 0 1 0 0 144 5 0.85 6.1 981 1.0 1.3 2.1 FDM10-8 FHWA 51 5 1 0 1 0 145 5 0.95 6.2 881 1.2 1.6 2.6 FDM11-1 FHWA 49 3 0 0 0 0 144 5 0.95 6.3 1461 1.0 1.2 1.6 FDM11-2 FHWA 49 3 1 1 1 0 145 5 0.85 6.5 581 1.3 1.8 3.8 FDM11-3 FHWA 49 5 0 1 1 0 135 5 0.95 6.2 1341 0.8 1.0 1.4 FDM11-4 FHWA 49 5 1 0 0 0 134 5 0.85 6.2 1081 0.9 1.2 1.8 FDM11-5 FHWA 51 3 0 0 1 0 144 5 0.85 6.5 961 1.2 1.5 2.2 FDM11-6 FHWA 51 3 1 1 0 0 135 5 0.95 6.4 1081 1.0 1.3 1.8 FDM11-7 FHWA 51 5 0 1 0 0 144 5 0.85 6.2 721 0.8 1.1 1.7 FDM11-8 FHWA 51 5 1 0 1 0 145 5 0.95 6.3 781 1.1 1.5 2.7 FDM12-1 AAT 49 3 0 0 0 0 145 4 0.90 6.6 1281 1.0 1.4 2.1 FDM12-2 AAT 49 3 1 1 1 0 145 10 0.90 6.4 901 0.9 1.3 2.2 FDM12-3 AAT 49 5 0 1 1 0 135 3 0.90 6.0 881 0.7 0.9 1.5 FDM12-4 AAT 49 5 1 0 0 0 135 12 0.90 6.4 1121 0.9 1.2 1.9 FDM12-5 AAT 51 3 0 0 1 0 135 10 0.90 6.3 581 0.8 1.3 2.8 FDM12-6 AAT 51 3 1 1 0 0 135 4 0.90 6.6 1041 1.1 1.6 2.5 FDM12-7 AAT 51 5 0 1 0 0 145 11 0.90 6.3 801 0.8 1.1 1.9 FDM12-8 AAT 51 5 1 0 1 0 145 3 0.90 6.1 641 1.1 1.6 3.2 FDM13-1 AAT 49 3 0 0 0 0 145 4 0.90 6.2 1021 0.9 1.2 1.7 FDM13-2 AAT 49 3 1 1 1 0 145 10 0.90 6.1 541 0.8 1.3 2.6 FDM13-3 AAT 49 5 0 1 1 0 135 4 0.90 6.2 781 0.8 1.1 1.9 FDM13-4 AAT 49 5 1 0 0 0 135 12 0.90 6.1 1101 1.1 1.5 2.1 FDM13-5 AAT 51 3 0 0 1 0 135 9 0.90 6.0 1061 1.1 1.4 2.1 FDM13-6 AAT 51 3 1 1 0 0 135 4 0.90 6.1 881 0.8 1.1 1.8

Friction ID Lab Temp Transfer Fluid End Reducer Confining Deviator Contact Dwell Air Flow Permanent Strain, % C Time 0=Water 0=Milled 0=Teflon Stress Stress Stress Time Void # 500 1000 2000 5000 8000 Min 1=Air 1=Sawed 1=Latex kPa kPa kPa sec % Cycles Cycles Cycles Cycles Cycles Cycles FDM13-7 AAT 51 5 0 1 0 0 145 11 0.90 6.1 621 0.7 0.9 1.6 FDM13-8 AAT 51 5 1 0 1 0 145 3 0.90 6.2 461 1.3 1.9 4.2 FDM6-1 AAT 49 3 0 0 0 135 984 5 0.90 6.1 2.4 2.9 3.3 FDM6-2 AAT 49 3 1 1 1 145 984 5 0.90 6.2 2.4 3.4 4.8 FDM6-3 AAT 49 5 0 1 1 135 944 5 0.90 6.0 1.9 2.3 2.8 FDM6-4 AAT 49 5 1 0 0 145 944 5 0.90 6.3 2.5 2.7 3.0 FDM6-5 AAT 51 3 0 0 1 145 944 5 0.90 6.0 2.4 2.7 3.2 FDM6-6 AAT 51 3 1 1 0 135 944 5 0.90 6.1 1.6 1.8 2.1 FDM6-7 AAT 51 5 0 1 0 145 984 5 0.90 6.1 1.6 1.8 2.1 FDM6-8 AAT 51 5 1 0 1 135 984 5 0.90 5.9 2.1 2.4 2.8 FDM8-1 AAT 49 3 0 0 0 135 984 5 0.90 6.2 2.1 2.3 2.6 FDM8-2 AAT 49 3 1 1 1 145 984 5 0.90 6.2 1.6 1.9 2.2 FDM8-3 AAT 49 5 0 1 1 135 944 5 0.90 6.0 1.6 1.8 2.1 FDM8-4 AAT 49 5 1 0 0 145 944 5 0.90 6.3 1.7 1.9 2.2 FDM8-5 AAT 51 3 0 0 1 145 944 5 0.90 6.5 2.7 3.0 3.3 FDM8-6 AAT 51 3 1 1 0 135 944 5 0.90 6.4 1.1 1.3 1.5 FDM8-7 AAT 51 5 0 1 0 145 984 5 0.90 6.0 1.4 1.6 1.8 FDM8-8 AAT 51 5 1 0 1 140 984 5 0.90 5.7 2.4 2.6 2.9 FDM7-1 FHWA 49 3 0 0 0 135 1048 45 0.90 6.1 1.7 2.0 2.3 FDM7-2 FHWA 49 3 1 1 1 145 1044 45 0.90 6.2 1.9 2.2 2.6 FDM7-3 FHWA 49 5 0 1 1 135 996 45 0.90 6.2 1.6 1.9 2.4 FDM7-4 FHWA 49 5 1 0 0 145 1009 46 0.90 6.3 1.5 1.7 2.0 FDM7-5 FHWA 51 3 0 0 1 145 991 45 0.90 6.4 1.9 2.4 2.9 FDM7-6 FHWA 51 3 1 1 0 135 1015 45 0.90 6.1 1.7 2.0 2.4 FDM7-7 FHWA 51 5 0 1 0 145 1049 45 0.90 6.4 1.8 2.2 2.6 FDM7-8 FHWA 51 5 1 0 1 135 1029 46 0.90 6.1 2.5 3.2 4.3 FDM9-1 FHWA 49 3 0 0 0 135 1052 45 0.90 6.1 2.0 2.4 2.9 FDM9-2 FHWA 49 3 1 1 1 145 1063 42 0.90 6.0 1.8 2.2 2.6 FDM9-3 FHWA 49 5 0 1 1 135 1002 44 0.90 6.3 2.0 2.5 3.2 FDM9-4 FHWA 49 5 1 0 0 145 1027 44 0.90 6.3 1.8 2.1 2.4

Friction ID Lab Temp Transfer Fluid End Reducer Confining Deviator Contact Dwell Air Flow Permanent Strain, % C Time 0=Water 0=Milled 0=Teflon Stress Stress Stress Time Void # 500 1000 2000 5000 8000 Min 1=Air 1=Sawed 1=Latex kPa kPa kPa sec % Cycles Cycles Cycles Cycles Cycles Cycles FDM9-5 FHWA 51 3 0 0 1 145 1010 42 0.90 6.0 2.4 3.0 3.6 FDM9-6 FHWA 51 3 1 1 0 135 1023 45 0.90 6.3 1.9 2.3 2.8 FDM9-7 FHWA 51 5 0 1 0 145 1052 45 0.90 6.1 2.2 2.7 3.3 FDM9-8 FHWA 51 5 1 0 1 135 1038 42 0.90 6.1 2.6 3.4 4.6 FSM5-1 AAT 49 3 0 0 0 135 1055 47 0.90 5.8 1.4 1.8 2.4 3.2 3.4 FSM5-2 AAT 49 3 1 1 1 145 1030 40 0.90 6.5 1.4 1.7 2.1 3.0 3.4 FSM5-3 AAT 49 5 0 1 1 135 1000 45 0.90 5.6 1.7 2.1 2.4 3.2 3.9 FSM5-4 AAT 49 5 1 0 0 145 1012 45 0.90 6.1 1.4 1.7 2.2 3.2 3.5 FSM5-5 AAT 51 3 0 0 1 145 1003 46 0.90 6.1 1.7 2.0 2.3 2.7 2.9 FSM5-6 AAT 51 3 1 1 0 135 1014 47 0.90 5.9 1.8 2.2 2.7 2.9 3.0 FSM5-7 AAT 51 5 0 1 0 145 1050 44 0.90 6.6 1.3 1.4 1.6 1.8 1.9 FSM5-8 AAT 51 5 1 0 1 135 1037 42 0.90 7.3 1.8 2.1 2.5 3.0 3.3 FSM6-1 AAT 49 3 0 0 0 135 1073 43 0.90 5.8 1.5 1.7 1.9 2.4 3.0 FSM6-2 AAT 49 3 1 1 1 145 1030 45 0.90 5.8 1.8 2.1 2.3 2.7 2.8 FSM6-3 AAT 49 5 0 1 1 135 995 44 0.90 5.7 2.1 2.5 2.9 3.6 4.2 FSM6-4 AAT 49 5 1 0 0 145 1010 47 0.90 5.8 1.4 1.5 1.7 2.1 2.5 FSM6-5 AAT 51 3 0 0 1 145 1007 45 0.90 5.6 1.9 2.1 2.4 2.9 3.4 FSM6-6 AAT 51 3 1 1 0 135 1010 46 0.90 5.4 1.3 1.4 1.7 2.4 3.2 FSM6-7 AAT 51 5 0 1 0 145 1052 47 0.90 5.8 1.8 2.2 3.1 4.4 4.6 FSM6-8 AAT 51 5 1 0 1 135 1034 44 0.90 5.4 2.3 2.8 3.4 3.8 3.9 FSM8-1 FHWA 49 3 0 0 0 135 984 5 0.90 6.0 1.2 1.3 1.4 1.5 1.6 FSM8-2 FHWA 49 3 1 1 1 145 984 5 0.90 5.8 1.5 1.7 1.8 2.0 2.1 FSM8-3 FHWA 49 5 0 1 1 135 944 5 0.90 5.5 1.5 1.6 1.9 3.2 4.3 FSM8-4 FHWA 49 5 1 0 0 145 944 5 0.90 5.6 0.9 1.1 1.3 1.7 2.0 FSM8-5 FHWA 51 3 0 0 1 145 944 5 0.90 5.4 1.4 1.6 1.7 2.1 3.0 FSM8-6 FHWA 51 3 1 1 0 135 944 5 0.90 5.7 1.1 1.4 1.6 1.9 2.1 FSM8-7 FHWA 51 5 0 1 0 145 984 5 0.90 5.4 0.9 1.0 1.1 1.2 1.3 FSM8-8 FHWA 51 5 1 0 1 135 984 5 0.90 5.5 1.9 2.2 2.7 3.5 3.7 FSM9-1 FHWA 49 3 0 0 0 135 984 5 0.90 6.5 1.5 1.6 1.8 2.2 2.8 FSM9-2 FHWA 49 3 1 1 1 145 984 5 0.90 6.2 1.6 1.8 2.3 3.3 3.9

Friction ID Lab Temp Transfer Fluid End Reducer Confining Deviator Contact Dwell Air Flow Permanent Strain, % C Time 0=Water 0=Milled 0=Teflon Stress Stress Stress Time Void # 500 1000 2000 5000 8000 Min 1=Air 1=Sawed 1=Latex kPa kPa kPa sec % Cycles Cycles Cycles Cycles Cycles Cycles FSM9-3 FHWA 49 5 0 1 1 135 944 5 0.90 6.0 1.8 2.0 2.1 2.4 2.6 FSM9-4 FHWA 49 5 1 0 0 145 944 5 0.90 5.9 1.2 1.3 1.6 2.1 2.4 FSM9-5 FHWA 51 3 0 0 1 145 944 5 0.90 5.7 1.4 1.6 1.8 2.2 2.6 FSM9-6 FHWA 51 3 1 1 0 135 944 5 0.90 5.8 1.2 1.5 1.8 2.4 2.5 FSM9-7 FHWA 51 5 0 1 0 145 984 5 0.90 5.5 1.2 1.5 2.0 3.3 3.7 FSM9-8 FHWA 51 5 1 0 1 135 984 5 0.90 5.8 1.6 1.9 2.3 3.1 3.8

Next: Appendix C - Dynamic Modulus Equipment Effects Data »
Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester Get This Book
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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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