ufc3-260-2Chapter 1. INTRODUCTION - ufc3-260-20016PAVEMENTDESIGN ANALYSIS - ufc3-260-20018Figure 1-1. Typical flexible pavement structureFigure 1-4. Typical rigid pavement structureChapter 2. ARMY AIRFIELD/HELIPORT REQUIREMENTSARMY AIRCRAFT DESIGN LOADS AND PASS LEVELSROLLER-COMPACTED CONCRETE PAVEMENTFigure 2-1. Typical layout of traffic areas for Army Class III and IV airfieldsChapetr 3. AIR FORCE AIRFIELD AND AGGREGATE SURFACED HELICOPTER SLIDE AREAS AND HELIPORT REQUIREMENTSTRAFFIC AREAS FOR AIR FORCE AIRFIELDSTRAFFIC AREAS FOR AIR FORCE AIRFIELDS - continuedType D Traffic AreasDESIGN PASS LEVELS FOR AIR FORCE PAVEMENTSTable 3-1. Design Gross Weights and Pass Levels for Airfield PavementsTable 3-2. Gradation for Aggregate Surface Courses (Percent Passing)Table 3-4. Frost Design Soil ClassificationTable 3-5. Frost Area Soil Support Indices (FASSI) of Subgrade SoilsSurface CourseTable 3-7. Compaction Requirements for Helicopter Pads and Slide AreasMaintenance - ufc3-260-20036Figure 3-1. Typical layout of traffic areas for Air Force light-load and auxiliary airfield pavementsFigure 3-2. Typical layout of traffic areas for Air Force medium- and modified-heavy- load airfield pavementsFigure 3-3. Typical layout of traffic areas for Air Force heavy-load airfield pavementsFigure 3-4. Aggregate surfaced design curves for helicoptersChapter 4. NAVY AND MARINE CORPS AIRFIELD REQUIREMENTSAIRCRAFT LOADINGSTable 4-1. Aircraft Characteristics and Design LoadingsTable 4-1. Aircraft Characteristics and Design Loadings - continuedTRAFFIC VOLUMEPAVEMENT DESIGN POLICYFigure 4-1. Primary, secondary, and supporting traffic areas for Navy and Marine Corps airfield pavementsFigure 4-2. Landing Gear assembliesChapter 5. SITE INVESTIGATIONSTable 5-1. Soil Sampling and Testing StandardsSELECT MATERIAL AND SUBBASE FOR FLEXIBLE PAVEMENTSSOIL COMPACTION TESTSFigure 5-1. Typical boring logFigure 5-2. Typical soil profileFigure 5-3. Approximate relationships of soil classification and soil strengthChapter 6. SUBGRADESUBGRADE CBRSUBGRADE MODULUS OF SOIL REACTIONtable 6-1. Typical Values of Modulus of Soil ReactionSUBGRADE COMPACTION FOR FLEXIBLE PAVEMENTS - NORMAL CASESTable 6-2. Compaction Requirements for Cohesive Subgrades and Select Materials Under Flexible Pavements - Air Force Pavements (LL>25; Pl > 5)Table 6-3. Compaction Requirements for Cohessionless Subgrades and Select Materials Under Flexible Pavements- Air Force PavementsTable 6-4. Compaction Requirements for Cohesive Subgrades and Select Materials under Flexible pavements - army pavementsTable 6-5. Comapction Requirements for Cohesionless subgrades and select materials under flexible pavements - army pavements (LL) > 25; Pl > 5Table 6-6. Compaction Requirements for Navy and Marine Corps Flexible PavementsTable 6-7. Compaction Requirements for ShouldersTREATMENT OF PROBLEM SOILSTREATMENT OF PROBLEM SOILS - continuedFigure 6-1. Procedure for determining laboratory CBR of subgrade soilsFigure 6-2. Selection of design subgrade CBR using in-place testsChapter 7. SELECT MATERIALS AND SUBBASE COURSES FOR FLEXIBLE PAVEMENTSTable 7-1. Minimum Unconfined Compressive Strength for Cement, Lime, Lime-Cement, and Lime-Cement-Fly Ash Stabilized SoilsSTABILIZED SELECT MATERIALS AND SUBBASESChapter 8. AGGREGATE BASE COURSESMATERIALS FOR AGGREGATE BASE COURSES IN FLEXIBLE PAVEMENTSAGGREGATE BASE COURSES FOR ARMY AND AIR FORCE RIGID PAVEMENTAGGREGATE BASE COURSES FOR NAVY AND MARINE CORPS RIGID PAVEMENTS.STRENGTH OF AGGREGATE BASE COURSES FOR RIGID PAVEMENTSTAble 8-1. Minimum Surface and Aggregate Base-Course Thickness Requirements for Army Flexible Pavement Airfields, InchesTable 8-5. Minimum Surface and Aggregate Base-Course Thickness Requirements for Air Force Flexible Pavement Airfields, InchesMINIMUM THICKNESS REQUIREMENTS FOR RIGID PAVEMENTS.COMPACTION REQUIREMENTS FOR ARMY AND AIR FORCE RIGID PAVEMENT AGGREGATE BASE COURSESFigure 8-1. Effect of base-course thickness on modulus of soil reaction for nonfrost conditionsChapter 9. PAVEMENT MATERIALSSTABILIZATIONSTABILIZATION - continuedDurability - ufc3-260-20087Sulfate attackDurability - ufc3-260-20089Suitable SoilsNontraditional StabilizersReinforcingSpecial Air Force RequirementSelection of Design StrengthPower Check Pads and Similar FacilitiesASPHALTIC CONCRETEASPHALTIC CONCRETE - continuedAging and OxidationTable 9-1. Types of Portland CementChpater 10. FLEXIBLE PAVEMENT DESIGN - CBR METHODADDITIONAL CONSIDERATIONS FOR THICKNESS DESIGN.DESIGN EXAMPLES.DESIGN EXAMPLES - continued - ufc3-260-20103DESIGN EXAMPLES - continued - ufc3-260-20104Table 10-1. Example Design Using Mixed TrafficAlternative designSPECIAL AREASTable 10-2. Equivalency Factors for Army and Air Force PavementsArmy AirfieldsShoulders.Figure 10-1. Flexible pavement design curves for Army Class I heliports and helipadsFigure 10-2. Flexible pavement design curves for Army Class II and V heliports and helipadsFigure 10-3. Flexible pavement design curves for Army Class III airfields as defined in paragraph 4.c of Chapter 2Figure 10-4. Flexible pavement design curves for Army Class IV airfields (C-130 aircraft) with runway # 1,525 meters (# 5,000 feet), type A traffic areasFigyre 10-5. Flexible pavement design curves for Army Class IV airfields (C-130 aircraft) with runway # 1,525 meters (# 5,000 feet), types B and C traffic areasFigure 10-6. Flexible pavement design curves for Army Class IV airfields (C-17 aircraft) with runway > 1,525 meters (> 5,000 feet), type A traffic areasFigure 10-7. Flexible pavement design curves for Army Class IV airfields (C-17 aircraft) with runway > 1,525 meters (> 5,000 feet), types B and C traffic areasFigure 10-9. Flexible pavement design curves for Navy and Marine Corps single- wheel aircraft, primary and secondary traffic areasFigure 10-9. Flexible pavement design curve for Navy and Marine Corps dual-Figure 10-8. Flexible pavement design curves for Navy and Marine Corps single-wheel aircraft, primary traffic areasFigure 10-10. Flexible pavement design curve for Navy and Marine Corps dual-wheel aircraft, secondary traffic areasFigure 10-11. Flexible pavement design curve for Navy and Marine Corps C-130, primary traffic areasFigure 10-12. Flexible pavement design curve for Navy and Marine Corps C-130, secondary traffic areasFigure 10-13. Flexible pavement design curve for Navy and Marine Corps C-141, primary traffic areasFigure 10-14. Flexible pavement design curve for Navy and Marine Corps C-141, secondary traffic areasFigure 10-15. Flexible pavement design curve for Navy and Marine Corps C-5A, primary traffic areasFigure 10-16. Flexible pavement design curve for Navy and Marine Corps C-5A, secondary traffic areasFigure 10-17. Flexible pavement design curve for Air Force light-load airfieldFigure 10-18. Flexible pavement design curve for Air Force medium-load airfieldTable 10-19. Flexible pavement design curve for Air Force heavy-load pavementFigure 10-20. Flexible pavement design curve for Air Force modified heavy-load pavementFigure 10-21a. Flexible pavement design curve for Air Force C-130 assault landing zone airfieldFigure 10-21b. Flexible pavement design curve for Air Force C-17 assault landing zone airfieldFigure10-22. Flexible pavement design curve for Air Force auxiliary airfield, type A traffic areasFigure 10-23. Flexible pavement design curve for Air Force auxiliary airfield, types B and C traffic areasFigure 10-24. Flexible pavement design curve for shoulders on Army and Air Force pavementsFigure 10-25. Air Force flexible pavement design curve for F-15, type A traffic areasFigure 10-26. Air Force flexible pavement design curve for F-15, types B and C traffic areasFigure 10-27. Air Force flexible pavement design curve for C-141, type A traffic areasFigure 10-28. Air Force flexible pavement design curve for C-141, types B, C, and D traffic areasFigure 10-29. Air Force flexible pavement design curves for B-1, type A traffic areasFigure 10-30. Air Force flexible pavement design curve for B-1, types B, C, and D traffic areasFigure 10-31. Air Force flexible pavement design curve for B-52, type A traffic areasFigure 10-32. Air Force flexible pavement design curve for B-52, types B, C, and D traffic areasChapter 11. LAYER ELASTIC DESIGN OF FLEXIBLE PAVEMENTSTable 11-1. Temperature Data for Jackson, MississippiTraffic DataTraffic groupingMATERIAL CHARACTERIZATIONSubgrade soilsTable 11-2. Typical Poisson's Ratios for Four Classes of Pavement MaterialsSubgrade Strain CriteriaCONVENTIONAL FLEXIBLE PAVEMENT DESIGNPAVEMENTS WITH A STABILIZED BASE COURSEEXAMPLE DESIGN FOR CONVENTIONAL FLEXIBLE PAVEMENTTable 11-3. Bituminous Concrete Moduli for Each Month for Conventional Flexible Pavement Design Based on Subgrade StrainTable 11-4. Bituminous Concrete Moduli for Each Month for Conventional Flexible Pavement Design Based on Bituminous Concrete StrainTable 11-5. Grouping Traffic into Traffic Groups According to Similar Asphalt ModuliTable 11-6. Structure Data File for Input into the JULEA Computer ProgramTable 11-6. Structure Data File for Input into the JULEA Computer Program - continuedComputation of Damage Factors.Table 11-8. Data File for Computing Subgrade Damage for Pavement Thicknesses of 840, 760, and 685 millimeters (33, 30, and 27 inches)Table 11-9. Program Output for Subgrade Damage for Pavement Thicknesses of 840, 760, and 685 millimeters (33, 30, and 27 inches)Table 11-10. Data File for Computing Asphalt DamageTable 11-11. Program Output for Asphalt DamageTable 11-12. Bituminous Concrete Moduli for Each Month for ABC Pavement Design Based on Bituminous Concrete StrainTable 11-13. Bituminous Concrete Moduli for Each Month for ABC Pavement Design Based on Subgrade StrainTable 11-14. Data for Computing Damage Factors for Taxiway DesignTable 11-15. Data for Computing Damage Factors for Runway DesignFigure 11-1. Temperature relationships for selected bituminous concrete thicknessFigure 11-2. Computation of effective gear print for single gearFigure 11-3. Computation of effective gear print for twin gearFigure 11-4. Computation of repetition factor for tandem gearFigure 11-5. Design criteria based on subgrade strainFigure 11-7. Flow diagram of important steps in design of bituminous concrete pavementFigure 11-8. Relationship between cracked section modulus and unconfined compressive strengthFigure 11-9. Flow diagram of important steps in design of pavements having chemically stabilized base course and unstabilized subbase courseFigure 11-10. Flow diagram of important steps in design of pavements having stabilized base and chemically stabilized subbase coursesFigure 11-11. Estimation of resilient modulus MRFigure 11-12. Results of laboratory tests for dynamic modulus of bituminous concreteFigure 11-13. Section for pavement thickness of 760 millimeters (30 inches) for initial taxiway designFigure 11-14. Section for pavement thickness of 610 millimeters (24 inches) for initial runway designFigure 11-15. Pavement design for taxiwaysFigure 11-16. Design for runwaysFigure 11-17. Design for asphalt concrete surfaceFigure 11-18. Computed strain at the top of the subgrade for taxiway designFigure 11-19. Damage factor versus pavement thicknessFigure 11-20. Computed strain at the bottom of the asphalt for taxiway designFigure 11-21. Computed strain at the top of the subgrade for runway designFigure 11-22. Computed strain at the bottom of the asphalt for runway designChapter 12. PLAIN CONCRETE PAVEMENTSTHICKNESS DESIGN - ARMY AND AIR FORCE PAVEMENTS.Example Design, Slab on Unbound BaseDesign Example for Mixed Traffic.Example problem solution.Table 12-1. Example of Mixed Traffic DesignStructural Slab Cracking and Mixed Aircraft LoadingTable 12-2. Stress-Strength Ratios and Allowable CoveragesThickness design procedure for a single design aircraftTable 12-3. Fatigue Damage Summary Sheet for Mixed TrafficTable 12-4. Pass-to-Coverage RatiosFatigue life consumptionSubgrade evaluation and testingSlab thickness and jointsTable 12-5. Design Example for Primary (Chamelized) Traffic AreasTable 12-5. Design Example for Primary (Chamelized) Traffic Areas - continuedTable 12-6. Design Example for Secondary (Unchamelized) Traffic AreasTable 12-6. Design Example for Secondary (Unchamelized) Traffic Areas - continuedJOINTS FOR ARMY AND AIR FORCE PAVEMENTSJOINTS FOR ARMY AND AIR FORCE PAVEMENTS - continuedTable 12-7. Recommended Spacing of Transverse Contraction JointsTable 12-8. Dowel Size and Spacing for Construction, Contraction, and Expansion JointsBetween pavement and structuresSpecial Provisions of Slipforming Paving.Construction JointsStabilized baseJOINTING PATTERN FOR RIGID AIRFIELD PAVEMENTSReplacements and AdditionsTied Joints (Navy Only)Sample Joint LayoutsSample Joint Layouts - continued - ufc3-260-20220Sample Joint Layouts - continued - ufc3-260-20221Figure 12-1. Plain concrete design curves for Army Helipads, Class IFigure 12-2. Plain concrete design curves for Army Class II airfieldsFigure 12-3. Plain concrete design curves for Army Class III airfields as defined in paragraph 4.c of Chapter 2Figure 12-4. Plain Concrete Curves for Army Class IV airfields (C-130 aircraft) with runway ≤ 1,525 meters (5,000 feet)Figure 12-5. Plain concrete design curves for army Class IV Airfields (C-17 aircraft) with runway >2,745 meters (9,000) feetFigure 12-6. Plain concrete design curves for Air Force light-load pavementsFigure 12-7. Plain concrete design curves for Air Force medium-load pavementsFigure 12-8. Plain concrete design curves for Air Force heavy-load pavementsFigure 12-9. Plain concrete design curves for Air Force modified heavy-load pavementsFigure 12-10. Plain concrete design curves for Air Force C-130 assault landing zone pavementsFigure 12-11. Plain concrete design curves for Air Force C-17 assault landing zoneFigure 12-12. Plain concrete design curves for Air Force auxiliary pavementsFigure 12-13. Plain concrete design curves for F-15 aircraftFigure 12-15. Plain concrete design curves for B-52 aircraftFigure 12-16. Plain concrete design curves for B-1 aircraftFigure 12-17. Plain concrete design curves for shouldersFigure 12-19. Rigid pavement thickness design chart for single-wheel load (Navy)Figure 12-20. Rigid pavement thickness design chart for P-3 aircraft (Navy)Figure 12-21. Rigid pavement thickness design chart for C-130 aircraft (Navy)Figure 12-22. Rigid pavement thickness design chart for C-141 aircraft (Navy)Figure 12-23. Rigid pavement thickness design chart for C-5A aircraft (Navy)Figure 12-24. Chart for determining flexural stress for single-wheel gear (Navy)Figure 12-25. Chart for determining flexural stress for P-3 aircraft (Navy)Figure 12-26. Chart for determining flexural stress for C-130 aircraft (Navy)Figure 12-27. Chart for determining flexural stress for C-141 aircraft (Navy)Figure 12-28. Chart for determining flexural stress for C-5A aircraft (Navy)Figure 12-29. Typical jointingFigure 12-30. Contraction joints for plain concrete pavementsFigure 12-31. Joint sealant details for plain concrete pavements (Sheet 1 of 3)Figure 12-31. (Sheet 2 of 3)Figure 12-31. (Sheet 3 of 3)Figure 12-32. Construction joints for plain concrete pavements (Sheet 1 of 3)Figure 12-32. Construction joints for plain concrete pavements (Sheet 2 of 3)Figure 12-32. Construction joints for plain concrete pavements (Sheet 3 of 3)Figure 12-33. Expansion joints for plain concrete pavementsFigure 12-34. Slip joints for plain concrete pavementsFigure 12-35. Regid-flexible pavement junction (Army or Air Force)Figure 12-36. Rigid-flexible pavement junctionFigure 12-37. PCC to AC joint detail (removal and construction)Figure 12-38. PCC to AC joint detail (very little traffic expected)Figure 12-39. Sample jointing pattern (SI units)Figure 12-40. Sample jointing pattern (metric units)Figure 12-41. Sample Jointing Pattern for 180-ft.-wide lanesFigure 12-42. Sample jointing pattern at an intersectionFigure 12-43. Effects of confusion in sawing jointsChapter 13. REINFORCED CONCRETE PAVEMENT DESIGNREDUCED THICKNESS DESIGN - ARMY AND AIR FORCE.Limitations to Reinforced Concrete Pavement Design ProcedureREINFORCEMENT TO CONTROL PAVEMENT CRACKING.REINFORCING STEEL.JOINTING.EXAMPLES OF REINFORCED CONCRETE PAVEMENT DESIGN.Table 13-1. Reinforced Concrete Pavement Design Example Table 13-2. Reinforced Concrete PavementDesign Example on a Lean Concrete Base CourseFigure 13-1. Reinforced concrete pavement designFigure 13-2. Typical layouts showing reinforcement of odd-shaped slabs and mismatched joints (Continued)Figure 13-2. Typical layouts showing reinforcement of odd-shaped slabs and mismatched joints (Concluded)Figure 13-3. Reinforcing steel details (Continued)Figure 13-3. Reinforcing steel details (Concluded)Figure 13-4. Contraction joints for reinforced concrete pavementsFigure 13-5. Construction joints for reinforced concrete pavements (Sheet 1 of 4)Figure 13-5. Construction joints for reinforced concrete pavements (Sheet 2 of 4)Figure 13-5. Construction joints for reinforced concrete pavements (Sheet 3 of 4)Figure 13-5. Construction joints for reinforced concrete pavements (Sheet 4 of 4)Figure 13-6. Expansion joints for reinforced concrete pavementsChapter 14. FIBROUS CONCRETE PAVEMENT DESIGNALLOWABLE DEFLECTION FOR FIBROUS CONCRETE PAVEMENTEXAMPLE OF FIBROUS CONCRETE PAVEMENT DESIGN.Figure 14-1. Fibrous concrete pavement design curves for UH-60Figure 14-2. Fibrous concrete pavement design curves for CH-47Figure 14-3. Fibrous concrete pavement design curves for C-130Figure 14-4. Fibrous concrete pavement design curves for Air Force light-load airfieldsFigure 14-5. Fibrous concrete pavement design curves for Air Force medium-load airfieldsFigure 14-6. Fibrous concrete pavement design curves for Air Force heavy-load airfieldsFigure 14-7. Fibrous concrete pavement design curves for Air Force modified heavy-load airfieldsFigure 14-8. Fibrous concrete pavement design curves for Air Force shortfield airfieldsFigure 14-9. Fibrous concrete pavement design curves for shouldersFigure 14-10. Deflection curves for UH-60Figure 14-11. Deflection curves for CH-47Figure 14-12. Deflection curves for C-130Figure 14-13. Deflection curves for Air Force light-load pavementsFigure 14-14. Deflection curves for Air Force medium-load pavementsFigure 14-15. Deflection curves for Air Force heavy-load pavementsFigure 14-16. Deflection curves for Air Force modified heavy-load pavementsFigure 14-17. Deflection curves for Air Force shortfield pavementsFigure 14-18. Deflection curves for shoulder pavementsFigure 14-19. Allowable deflection curves for fibrous concrete pavementsFigure 14-19. Allowable deflection curves for fibrous concrete pavements - concludedChapter 15. CONTINUOUSLY REINFORCED CONCRETE PAVEMENT DESIGNREINFORCING STEEL DESIGN.REINFORCING STEEL DESIGN - conitnuedJOINT SEALING - ufc3-260-20313EXAMPLE OF CONTINUOUSLY REINFORCED CONCRETE PAVEMENT DESIGNEXAMPLE OF CONTINUOUSLY REINFORCED CONCRETE PAVEMENT DESIGN - continuedFigure 15-1. Details of a wide-flange beam jointChapter 16. PRESTRESSED CONCRETE PAVEMENT DESIGNDESIGN PROCEDURE.DESIGN PROCEDURE - continuedPRESTRESSING TENDON DESIGN.PRESTRESSING TENDON DESIGN - continuedJOINTINGEXAMPLES OF PRESTRESSED CONCRETE PAVEMENT DESIGNEXAMPLES OF PRESTRESSED CONCRETE PAVEMENT DESIGN - continued - ufc3-260-20324EXAMPLES OF PRESTRESSED CONCRETE PAVEMENT DESIGN - continued - ufc3-260-20325Figure 16-1. Stress repetitions versus load repetition factorFigure 16-2. A/R2 versus load-moment factorFigure 16-3. Ratio of multiple wheel gear to single-wheel gear load versus A/R2Figure 16-4. Typical section of transverse jointsFigure 16-5. Typical transverse joint seals (Sheet 1 of 3)Figure 16-5. Typical transverse joint seals (Sheet 2 of 3)Figure 16-5. Typical transverse joint seals (Sheet 3 of 3)design prestressChapter 17. OVERLAY PAVEMENT DESIGNSITE INVESTIGATIONSPREPARATION OF EXISTING PAVEMENT.CONDITION OF EXISTING CONCRETE PAVEMENT.CONDITION OF EXISTING CONCRETE PAVEMENT - continuedRIGID OVERLAY OF EXISTING RIGID PAVEMENT.RIGID OVERLAY OF EXISTING RIGID PAVEMENT - continued - ufc3-260-20340RIGID OVERLAY OF EXISTING RIGID PAVEMENT - continued - ufc3-260-20341RIGID OVERLAY OF EXISTING RIGID PAVEMENT - continued - ufc3-260-20342RIGID OVERLAY OF EXISTING RIGID PAVEMENT - continued - ufc3-260-20343RIGID OVERLAY OF EXISTING RIGID PAVEMENT - continued - ufc3-260-20344NONRIGID OVERLAY OF EXISTING RIGID PAVEMENT.NONRIGID OVERLAY OF EXISTING RIGID PAVEMENT - continuedTable 17-1. Pass per Coverage RatiosNONRIGID OVERLAY ON FLEXIBLE PAVEMENTNONRIGID OVERLAY ON FLEXIBLE PAVEMENT - continuedOVERLAYS IN FROST REGIONSFigure 17-1. Structural condition index versus condition factorFigure 17-2. Factor for projecting cracking in a flexible pavementFigure 17-3. Location guide for the use of geotextiles in retarding reflective crackingChapter 18. RIGID PAVEMENT INLAY DESIGNRIGID INLAYS IN EXISTING RIGID PAVEMENT.Figure 18-1. Typical rigid pavement inlay in existing flexible pavementFigure 18-2. Typical rigid pavement inlay in existing rigid pavementChapter 19. LAYER ELASTIC DESIGN OF RIGID PAVEMENTSMATERIAL CHARACTERIZATION.Bound Bases (Subbases).Table 19-1. Recommended Maximum Stress Levels to Test Bituminous-Stabilized MaterialsUnbound (Granular) Bases (Subbases).Subgrade Soils.DESIGN CRITERIA.FROST CONSIDERATIONBase Slab Pavement Fatigue and Structural ConditionTime PeriodsDESIGN EXAMPLES - ufc3-260-20368DESIGN EXAMPLE 1, SINGLE AIRCRAFTDESIGN EXAMPLE 2, MIXED AIRCRAFT TRAFFICTable 19-5. Characteristics of Design AircraftTable 19-6. Computation of Cumulative Damage for Mixed Traffic, 10-inch Stabilized Base CoursesTable 19-7. Relationship Between Cumulative Damage and PCC Thickness for Mixed TrafficDESIGN EXAMPLE 4, ALTERNATE OVERLAY DESIGN PROCEDURETable 19-8. Data for Overlay Design, Example 4 (BAse Slab Calculations)Table 19-9. Time Intervals for the 356-millimeter (14-inch) OverlayTable 19-10. Computation of the Cumulative Damage for the 14-inch OverlayTable 19-10. Computation of the Cumulative Damage for the 14-inch Overlay - concludedFigure 19-1. Diagram for design of airfield rigid pavementsby layered elastic theoryFigure 19-2. Correlation between resilient modulus of elasticity and static modulus of soil reactionFigure 19-3. Relationship between SCI and coverages at initial cracking and complete failureFigure 19-5. Composite overlay performance curveFigure 19-7. Effect of steel reinforcement on rigid pavementsFigure 19-8. Relationship between cumulative damage and concrete slab thickness for granular and stabilized bases (see Design Example 1)Figure 19-9. Relationship between cumulative damage and pavement thickness, mixed aircraft traffic (see Design Example 2)Figure 19-10. Base slab performance curve for the 356-millimeter (14-inch) overlayFigure 19-12. Cumulative damage plot for the 356-millimeter (14-inch) overlayFigure 19-14. Plot showing the overlay thickness versus the overlay lifeChapter 20. SEASONAL FROST CONDITIONSTable 20-1. Frost Design ClassificationTable 20-2. Frost Susceptibility ClassificationTable 20-3. Frost Area Soil Support Indexes (FASSI) for Subgrade SoilsRigid Pavement Thickness DesignRigid Pavement Thickness Design - continuedLIMITED SUBGRADE FROST PENETRATION METHODLIMITED SUBGRADE FROST PENETRATION METHOD - continued - ufc3-260-20396LIMITED SUBGRADE FROST PENETRATION METHOD - continued - ufc3-260-20397GRANULAR BASE- AND SUBBASE-COURSE REQUIREMENTSDRAINAGE LAYER REQUIREMENTSSUBGRADE REQUIREMENTSCONTROL OF DIFFERENTIAL HEAVE AT DRAINS, CULVERTS, DUCTS, INLETS, HYDRANTS, AND LIGHTSPAVEMENT THICKNESS TRANSITIONS.FLEXIBLE PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS.FLEXIBLE PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continuedRIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONSRIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20406RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20407RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20408RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20409RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20410RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20411RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20412RIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - conitnuedRIGID PAVEMENT DESIGN EXAMPLES FOR SEASONAL FROST CONDITIONS - continued - ufc3-260-20414Figure 20-1. Frost area index of reaction (FAIR) for design of rigid pavementsFigure 20-2. Determination of freezing indexFigure 20-3. Distribution of design freezing indexes in North AmericaFigure 20-4. Distribution of mean freezing indexes in Northern EurasiaFigure 20-5. Frost penetration beneath pavementsFigure 20-6. Design of combined base thickness for limited subgrade frost penetrationFigure 20-7. Placement of drainage layer in frost areasFigure 20-8. Tapered transition used where embankment material differs from natural subgrade in cutFigure 20-9. Subgrade details for cold regionsFigure 20-10. Transitions for culverts beneath pavementsFigure 20-11. Relationship between base course thickness and PCC thickness for example 1Figure 20-12. Relationship between base course thickness and PCC thickness for example 2Chapter 21. IMPROVING SKID RESISTANCE/REDUCING HYDROPLANING POTENTIAL OF RUNWAYSIMPROVING RUNWAY FRACTION CHARACTERISTICSFigure 21-1. Groove configuration for airfieldsAppendix A. REFERENCES - ufc3-260-20430Appendix A. REFERENCES - continued - ufc3-260-20431Appendix A. REFERENCES - continued - ufc3-260-20432Appendix A. REFERENCES - continued - ufc3-260-20433Appendix A. REFERENCES - continued - ufc3-260-20434Appendix A. REFERENCES - continued - ufc3-260-20435Appendix A. REFERENCES - continued - ufc3-260-20436Appendix A. REFERENCES - continued - ufc3-260-20437Appendix B. AIRFIELD/HELIPORT DESIGN ANALYSIS OUTLINESITE DESCRIPTION - ufc3-260-20439TESTINGPAVEMENT THICKNESS DESIGN CRITERIAPAVEMENT THICKNESS DESIGN - ufc3-260-20442AIRFIELD LIGHTING AND NAVAIDS IMPROVEMENTSLIST OF REQUIRED WAIVERSAppendix C. RECOMMENDED CONTRACT DRAWING OUTLINE FOR AIRFIELD/HELIPORT PAVEMENTSPHASING PLAN AND DETAILS.BORING LOCATION PLAN AND BORING LOG DATAEXISTING UTILITIES PLANPLAN AND PROFILE SHEETS.REINFORCING DETAILSAppendix D. WAIVER PROCESSING PROCEDURESAdditional RequirementsEffective Length of WaiverBase Civil EngineerApprovalAppendix E. DETERMINATION OF FLEXURAL STRENGTH AND MODULUS OF ELASTICITY OF BITUMINOUS CONCRETETEST PROCEDURES - ufc3-260-20457CALCULATIONS - ufc3-260-20458Appendix F. CURVES FOR DETERMINING EFFECTIVE STRAIN REPETITIONSFigure F-2.Effective repetitions of strain for UH-60 aircraft, type A or primary traffic areasFigure F-3. Effective repetitions of strain for CH-47 aircraft, types B, C, or secondary traffic areasFigure F-4. Effective repetitions of strain for CH-47 aircraft, type A or primary traffic areasFigure F-5. Effective repetitions of strain for OV-1 aircraft, types B, C, or secondary traffic areasFigure F-6. Effective repetitions of strain for OV-1 aircraft, type A or primary traffic areasFigure F-7. Effective repetitions of strain for C-12 aircraft, types B, C, or secondary traffic areasFigyre F-8. Effective repetitions of strain for C-12 aircraft, type A or primary traffic areasFigure F-9. Effective repetitions of strain for C-130 aircraft, types B, C, or secondary traffic areasFigure F-10. Effective repetitions of strain for C-130 aircraft, type A or primary traffic areasFigure F-11. primary traffic areas types B and C traffic areasFigure F-12. Effective repetitions of strain for F-15 aircraft, Air Force type A traffic areasFigure F-13. Effective repetitions of strain for F-14 aircraft, types B, C and secondary traffic areasFigure F-14. Effective repetitions of strain for F-14 aircraft, type A or primary traffic areasFigure F-15. Effective repetitions of strain for B-52 aircraft, types B, C or secondary traffic areasFigure F-16. Effective repetitions of strain for B-52 aircraft, type A or primary traffic areasFigure F-17. Effective repetitions of strain for B-1 and C-141 aircraft, types B, C, or secondary traffic areasFigure F-18. Effective repetitions of strain for B-1 and C-141 aircraft, type A or primary traffic areasFigure F-19. Effective repetitions of strain for P-3 aircraft, types B, C, or secondary traffic areasFigure F-20. Effective repetitions of strain for P-3 aircraft, type A or primary traffic areasFigure F-21. Effective repetitions of strain for C-5 aircraft, types B, C, or secondary traffic areasFigure F-22. Effective repetitions of strain for C-5 aircraft, type A or primary traffic areasAppendix G. PROCEDURE FOR PREPARATION OF BITUMINOUS CYLINDRICAL SPECIMENSPROCEDURE.Appendix H. PROCEDURE FOR DETERMINING THE DYNAMIC MODULUS OF BITUMINOUS CONCRETE MIXTURESPROCEDURE - ufc3-260-20484CALCULATIONS - ufc3-260-20485Appendix I. PROCEDURE FOR ESTIMATING THE MODULUS OF ELASTICITY OF BITUMINOUS CONCRETESTEPS OF PROCEDUREFigure I-1. Relationship between penetration at 25 degrees C and ring-and-ball softening point for bitumens with different PI'sFigure I-2. Nomograph for determining the stiffness modulus of bitumensAppendix J. PROCEDURE FOR DETERMINING THE MODULUS OF ELASTICITY OF UNBOUND GRANULAR BASE AND SUBBASE COURSE MATERIALSEXAMPLESFigure J-1. Relationships between modulus of layer n and modulus of layer n + 1 for various thicknesses of unbound base course and subbase courseFigure J-3. Modulus values determined for second exampleAppendix K. PROCEDURE FOR DETERMINING THE FLEXURAL MODULUS AND FATIGUE CHARACTERISTICS OF STABILIZED SOILSTest ProcedureGRAPHICAL DETERMINATION OF FLEXURAL MODULUS FOR CHEMICALLY STABILIZED SOILS (CRACKED SECTION)Figure K-2. Details of equipment setupFigure K-3. Miscellaneous detailsAppendix L. PROCEDURE FOR DETERMINING RESILIENT MODULUS OF SUBGRADE MATERIALPREPARATION OF SPECIMENSPREPARATION OF SPECIMENS - continuedSoils Containing GravelQ TEST WITH BACK-PRESSURE SATURATIONBack-Pressure ProcedureEQUIPMENT - ufc3-260-20505PREPARATION OF SPECIMENS AND PLACEMENT IN TRIAXIAL CELL - ufc3-260-20506RESILIENCE TESTING OF COHESIVE SOILSRESILIENCE TESTING OF COHESIONLESS SOILS.INTERPRETATION OF TEST RESULTSINTERPRETATION OF TEST RESULTS - continuedFigure L-1. Schematic diagram of typical triaxial compression apparatusFigure L-2. Triaxial cellFigure L-3. LVDT clampsFigure L-4. Presentation of results of resilience tests on cohesive soilsFigure L-5. Presentation of results of resilience tests on cohesionless soilsFigure L-6. Estimated deviator stress at top of subgradeFigure L-7. Determination of subgrade modulus for cohesive soilsFigure L-8. Relationship for estimating 2 due to overburdenFigure L-9. Estimated θ at top of subgradeFigure L-10. Seclection of MRfor silty-sand subgrade with estimated thickness of 762 millimiters (30 inches) for 100,000 repitition ofs strainAppendix M. PROCEDURES FOR DETERMINING THE FATIGUE LIFE OF BITUMINOUS CONCRETELABORATORY TEST METHODReport and Presentation of ResultsFigure M-1. Repeated flexure apparatusFigure M-2. Initial mixture bending strain versus repetitions to fracture in controlled stress testsFiure M-3. Provisional fatigue data for bituminous base-course materialsAppendix N. PROCEDURE FOR DETERMINING THE RESILIENT MODULUS OF GRANULAR BASE MATERIALEQUIPMENT - ufc3-260-20528PREPARATION OF SPECIMENS AND PLACEMENT IN TRIAXIAL CELL - ufc3-260-20529PREPARATION OF SPECIMENS AND PLACEMENT IN TRIAXIAL CELL - continuedCOMPUTATIONS AND PRESENTATION OF RESULTS.COMPUTATIONS AND PRESENTATION OF RESULTS - continuedFigure N-1. Triaxial cell used in resilience testing of granular base materialFigure N-2. Schematic of frictionless cap and baseFigure N-3. Details of Top LVDT ring clampFigure N-4. Details of bottom LVDT ring clampFigure N-5. Representation of results of resilience test on cohesionless soils