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Rights & Permissions Free PDF Access Sign in to download PDF book and chapters Free Resources Display this book on your site! Related Titles NCHRP Report 614: Refining the Simple Performance Tester for Use in Routine Practice NCHRP Web Doc 14 Laboratory Determination of Resilient Modulus for Flexible Pavement Design:Final Report Other Related Titles NCHRP Report 629: Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester (2008) National Cooperative Highway Research Program (NCHRP) Citation Manager Export the bibliographic data for this book in your chosen format Web Search Builder Use this book's key terms to search within this book, across our collection, or across the Web. Skim This Chapter Skim this chapter and use this chapter's key terms to search within this book. Reference Finder Paste in your own text to find books that relate to your topic. Citation Manager Bonaquist, Ramon F, Transportation Research Board. "Appendix B - Flow Number Ruggedness Data." NCHRP Report 629: Ruggedness Testing of the Dynamic Modulus and Flow Number Tests with the Simple Performance Tester. Washington, DC: The National Academies Press, 2008. Please select a format: Page 49   E-mail Share on facebook Facebook Share on delicious Delicious Share on stumbleupon Stumble Share on twitter Twitter More Sharing ServicesMore Page 49 Front Matter (R1-R10) Summary (1-1) 1.2 Scope (2-2) 1.3.1 Background (3-3) 1.3.2 Ruggedness Testing Plan for Dynamic Modulus (4-6) 1.3.3 Ruggedness Testing Plan for the Flow Number Tests (7-9) 1.4 Equipment Effects Experiment (10-11) 2.2 Dynamic Modulus Test (12-12) 2.2.1 Factors Affecting Dynamic Modulus and Phase Angle (13-14) 2.2.2 Factors Affecting Data Quality Indicators (15-18) 2.2.3 Summary (19-19) 2.3.1 Factors Affecting Flow Number (20-21) 2.3.2 Factors Affecting Permanent Strain (22-23) 2.3.3 Summary (24-26) 3.2.1 Equipment Modifications (27-27) 3.2.2 Statistical Analysis (28-31) 3.3 Flow Number (32-32) 3.3.1 Statistical Analysis (33-34) 3.4 Repeatability (35-35) 3.5 Summary (36-36) 4.2 SPT Test Methods Modifications (37-37) 4.3 Manufacturer Modifications (38-38) References (39-39) Appendix A - Dynamic Modulus Ruggedness Data (40-48) Appendix B - Flow Number Ruggedness Data (49-53) Appendix C - Dynamic Modulus Equipment Effects Data (54-60) Appendix D - Flow Number Equipment Effects Data (61-66) Appendix E - Final Version of the SPT Equipment Specifications (67-111) Appendix F - SPT Test Methods (112-126) Abbreviations used without definitions in TRB publications (127-127)

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B1 APPENDIX B Flow Number Ruggedness Data

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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

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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

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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

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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