AAR-410 February 2, 20051 Alpha Factor Determination for 6-Wheel Gears u Gordon Hayhoe, AAR-410, FAA William J. Hughes Technical Center, Atlantic City,

Slides:



Advertisements
Similar presentations
Presented to: By: Venue: Date: Federal Aviation Administration 10-Year Airport Pavement R&D Plan Airport Pavement Working Group Gordon Hayhoe, ANG-E262.
Advertisements

CC-5: Post-Traffic Testing FAA Working Group Meeting DATE : April 24, 2012 By: Harkanwal Brar.
FAA Airport Technology Research & Development Program Air Transport Committee ASCE National Capitol Section March 22, 2005.
AAR /13/031 FAA Airport Pavement Technology Program u Testing and preliminary data analysis from flexible pavements on low-strength subgrade (Construction.
Construction and Testing of Construction Cycle 2 (CC2) Overlay Murphy Flynn FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center,
Federal Aviation Administration William J. Hughes Technical Center AIRPORTSAFETYTECHNOLOGYRESEARCH 29 th Annual Airport Conference February 28 – March.
Pavement Design Session Matakuliah: S0753 – Teknik Jalan Raya Tahun: 2009.
O’Hare Modernization Project Reflective Cracking and Improved Performance of Grooved Asphalt July 20 th, 2006 Research Overview Hyunwook Kim, Research.
Binder Characterizations for High Tire Pressure Project 04/26/2012 Injun Song Injun Song, Ph.D., P. E. SRA International, Inc. Federal Aviation Administration.
ICAO-UPDATE, ACN/PCN Federal Aviation Administration
Pavement Design CE 453 Lecture 28.
COMFAA 3.0 Update Airport Pavement Working Group
1 Characterization of Granular Base Materials for Design of Flexible Pavements Lulu Edwards, Walter Barker, Don Alexander US Army Engineer Research and.
Tranlation: EASL’s Average Daily Traffic Time or Traffic Pavement Condition Index Pavement Performance Pavement Condition High Performance Intersections.
Know the factors considered in the AASHTO design method
Pavement Design.
FDOT Aviation Pavement Inspection Training Module 2 – Pavement Fundamentals – Overview Florida Department of Transportation Statewide Pavement Management.
In Tai Kim & Erol Tutumluer University of Illinois, Urbana-Champaign
Vehicle and Traffic Consideration CEE 320 Steve Muench 5/9/ Highways Airports.
Monty Wade, P.E Applied Pavement Technology, Inc. April 4, 2012
FAA/Asphalt Institute Airport Pavement Workshop October 18-20, 2011 Newport Beach, California The Benefit of Runway Grooving Hector Daiutolo 1.
PAVEMENT DESIGN. Introduction Pavement design is the major component in the road construction. Nearly one-third or one-half of the total cost of construction,
PERMANENT DEFORMATION BEHAVIOR OF THE GRANULAR LAYERS TESTED AT THE FAA’s NATIONAL AIRPORT PAVEMENT TEST FACILITY NAVNEET GARG, Ph.D. Senior Research Engineer,
PRACTICAL AIRPORT PAVEMENT M&R MANAGEMENT Y. Hachiya & M. Kanno Service Center of Port Engineering Tokyo, JAPAN 1 FAA Airport Pavement Working Group Meeting.
Evaluation of Subbase Compaction Characteristics Craig Kumpel Andrew Melici Stephen Rossi Colin Yurick Dr. Beena Sukumaran FAA Working Group Meetings,
Gordon F. Hayhoe FAA AAR-410
TRB AFK10 Committee on General Issues in Asphalt Technology Update on NCAT Test Track and Other Research Results April 24-26, 2006.
Lec 28, Ch.20, pp : Flexible pavement design, ESAL (Objectives)
Load Characterization. Rigid Pavement Design Course Traffic Load Considerations Load Groups Lane Wander Load Configuration.
Bituminous Stabilized Materials Guideline Project Initiated By: Gautrans Sabita.
Flexible Pavement FAARFIELD Design Example
Pavement Base & Subbase CEE 320 Steve Muench 8/13/ The subbase course is between the base course and the subgrade. It functions primarily as structural.
COMFAA 3.0 Beta.
February 1, Analysis of Test Slab Failure Data David R. Brill FAA Airport Technology R&D Branch, AAR-410 William J. Hughes Technical Center, Atlantic.
JOINT LOAD TRANSFER EFFICIENCY OF RIGID PAVEMENT CONSIDERING DYNAMIC EFFECTS UNDER A SINGLE MOVING LOAD Xinhua YU, Yumin ZHOU, Zhiming TAN Tongji University,
Presented to: By: Date: Federal Aviation Administration National Airport Pavement Test Facility Update Airport Pavement Working Group Don Barbagallo April.
APPLICATIONS OF ENERGY CONCEPTS FOR FATIGUE ANALYSIS OF AIRPORT PAVEMENTS FAA Fatigue Project Briefing October 7th, 2004 Urbana, IL Samuel H. Carpenter,
Status of the first experiment at the PaveLab Fabricio Leiva-Villacorta, PhD Jose Aguiar-Moya, PhD Luis Loria-Salazar, PhD August 31 st, 2015.
THE DESIGN OF POROUS PAVEMENT SHOULDERS AT RICHMOND INTERNATIONAL AIRPORT 33 rd Annual Airports Conference March 3, 2010 – Hershey, PA Presented by: H.
ASTM E17 Committee Mini-Seminar Dec. 5, 2006 Federal Aviation Administration 1 FAA PERSPECTIVE Airfield Pavement Roughness Presentation to: ASTM E17 Committee.
Evaluation of Subbase using the Superpave Gyratory Compactor
Skip Hudspeth and Gordon Hayhoe 112/20/2015. Pavement Roughness Subjective Pilot Rating Study Phase I - Develop a surface roughness model on the B
HIGH TIRE PRESSURE AND TEMPERATURE EFFECTS ON HOT MIX ASPHALT CONCRETE PERMANENT DEFORMATION USING CUSTOMIZED ASPHALT PAVEMENT ANALYZER April 22, 2010.
DESIGN FLEXIBLE AND RIGID PAVEMENTS Ms Ikmalzatul Abdullah.
Presented to: 2010 FAA Worldwide Airport Technology Transfer Conference By: Gordon Hayhoe, FAA AJP-6312, WJHTC Date: April 20, 2010 Federal Aviation Administration.
AAR-410 January 14, FAA Airport Pavement Technology Program u National Airport Pavement Test Facility, FAA William J. Hughes Technical Center, Atlantic.
Using Reflective Crack Interlayer-
Presented to: FAA Airport Pavement Working Group Meeting By: David R. Brill, P.E., Ph.D. Date: April 24, 2012 Federal Aviation Administration Update on.
TRANSPORTATION ENGINEERING-II
Asphalt Technology Course
Presented to: By: Date: Federal Aviation Administration Full-Scale Testing Overload Update REDAC Subcommittee on Airports David R. Brill, P.E., Ph.D. March.
Presented to: REDAC By: Navneet Garg, Ph.D. Date: March 15, 2016 Federal Aviation Administration RPA P2: National Airport Pavement & Materials Research.
Overview of dTIMS Input, Analysis and Reporting HTC INFRASTRUCTURE MANAGEMENT LTD.
Presented to: REDAC By: Navneet Garg, Ph.D. Date: March 15, 2016 Date: March 15, 2016 Federal Aviation Administration Full-Scale Testing – Perpetual Pavement.
Airport Pavements Lexington, KY.
Tensar TriAx TX8 Geogrid
Phase I Experiment 4 Different pavement structures, 8 sections Compare
Presenters: Sumon Roy1 and Badrul Ahsan1
Chapter(16) AASHTO flexible pavement design method
Center of Excellence for Airport Technology, CEAT
Pavement Design  A pavement consists of a number of layers of different materials 4 Pavement Design Methods –AASHTO Method –The Asphalt Institute Method.
Introduction to Pavement Design
Erol Tutumluer & In Tai Kim University of Illinois, Urbana-Champaign
Calculating Dimensions for a Typical Pavement Section using 1993 AASHTO Flexible Pavement Design Guide.
Flexible Pavement Design (JKR Method)
HVS Testing at ERDC – Last Five Years
Flexible pavement design
Pavement Structural Analysis
Pavement Overlay Design
Louisiana Accelerated Pavement Research Facility
Presentation transcript:

AAR-410 February 2, Alpha Factor Determination for 6-Wheel Gears u Gordon Hayhoe, AAR-410, FAA William J. Hughes Technical Center, Atlantic City, New Jersey, U.S.A. u Need for evaluation u Full-scale test structures and results u Procedure for calculating alpha factors u Alpha factor Proposals for consideration by ICAO u Implications for thickness design

AAR-410 February 2, B-777 Six-Wheel ACNs u For flexible pavements, the ACNs initially computed for B wheel gears appeared to be unreasonably high. u The FAA had similar concerns about the existing CBR method for 6-wheel gears. u A380 also has 6-wheel body gears.

AAR-410 February 2, Alpha Factors – MWHGL Data

AAR-410 February 2, Interim 6-Wheel Alpha Factor at 10,000 Coverages u 4-Wheel alpha = u “Original” 6-wheel alpha = (inception to 1995) u “Interim” 6-wheel alpha = 0.72 (1995 to present) u Current 12-wheel alpha = 0.722

AAR-410 February 2, Alpha Factors – MWHGL Data C5-A as one 12-wheel gear C5-A as two 6-wheel gears

AAR-410 February 2, National Airport Pavement Test Facility (NAPTF) for 6-Wheel Tests u Joint FAA and Boeing. u Testing is funded and conducted entirely by the FAA. u Tests run on flexible test items to compare 4-wheel and 6-wheel gears. u Construction cycles CC1 etc.

AAR-410 February 2, NAPTF Construction Cycles u CC1 = original construction. u Conventional and stabilized base flexible on low- strength subgrade (LFC and LFS). u Conventional and stabilized base flexible on medium- strength subgrade (MFC and MFS). u CC2 = rigid pavements, trafficking completed. u CC3 = flexible pavement reconstruction with four conventional test items, trafficking and posttraffic testing completed.

AAR-410 February 2, CC3 Test Pavements - Profile Direction of Traffic

AAR-410 February 2, North, 6-Wheel Track LFC1 LFC2 LFC3 LFC4

AAR-410 February 2, Trench in LFC2 Flexible

AAR-410 February 2, Computation of Alpha Factor u Pass/Coverage ratios calculated from surface coverages in test wander pattern: u 4-Wheel = 2.36 for CC3 and 2.06 for CC1 u 6-Wheel = 1.57 u Subgrade CBR = trench measurements. u Total structure thicknesses are known. u Contact area = 265 square inches. u Compute Alpha using COMFAA.

AAR-410 February 2, CBR Equations Post-MWHGL equation: t =  (A c ) 0.5 [ – (log CBR/P) – (log CBR/P) 2 – (log CBR/P) 3 ] Pre-MWHGL equation: Solve the Post-MWHGL equation for  OR t = Total Thickness P = ESWL

AAR-410 February 2, Change the Input Alpha until the design thickness is equal to the test structure thickness.

AAR-410 February 2, MWHGL Subgrade CBR Measurements u The CBR of the subgrade for each MWHGL test item was calculated from all available measurements: u After construction, before traffic. u Trench and pit after traffic at surface, 12-inch, and 24-inch depth.

AAR-410 February 2, Summary of NAPTF Flexible Pavement Full-Scale Test Results * Extrapolated from rut depth curve Bold = corrected values

AAR-410 February 2, NAPTF and MWHGL Alpha Factor Results (No conversion of NAPTF to MWHGL structures)

AAR-410 February 2, LEDFAA 1.3 Flexible Failure Model

AAR-410 February 2, NAPTF versus MWHGL Test Results u NAPTF pavements tended to last longer than MWHGL pavements. Possible reasons for this are: u Indoor NAPTF operation means lower asphalt temperatures. u NAPTF asphalt and base layers are thicker. u NAPTF subbase material is of higher quality (strength – screenings versus uncrushed aggregate).

AAR-410 February 2, Procedure for Converting NAPTF Structures to Equivalent MWHGL Structures (Example) (a) real structure, 29.0 in. (b) convert 2 in. AC to 3.2 in. CA (E.F. 1.6) (c) add 3.2 in. CA to exist. 8 in. CA = 11.2 in. CA (d) convert 5.2 in. CA to 8.3 in. SQS (E.F. 1.6) (e) convert 16 in. HQS to 19.2 in. SQS (E.F. 1.2) (f) equivalent MWHGL structure, 36.5 in. Steps:

AAR-410 February 2, NAPTF Flexible Pavement Equivalent Thicknesses and Alpha Factors

AAR-410 February 2, NAPTF and MWHGL Alpha Factor Results (With conversion of NAPTF to MWHGL structures)

AAR-410 February 2, NAPTF and MWHGL Alpha Factor Results No structure conversions and C5-A as two 6-wheel gears NAPTF structures converted to equivalent MWHGL structures (SQS = 1.6 x CA) and C5-A as two 6-wheel gears

AAR-410 February 2, and 6-Wheel Alpha Factors for Base-to-Subbase Equivalency = 1.4 Alpha factor quadratic curve fit intercepts at 10,000 coverages: 4-wheel  = wheel  = From MWHGL report: 4-wheel  = wheel  = 0.788

AAR-410 February 2, and 6-Wheel Alpha Factors for Base-to-Subbase Equivalency = 1.6 Alpha factor quadratic curve fit intercepts at 10,000 coverages: 4-wheel  = wheel  = From MWHGL report: 4-wheel  = wheel  = 0.788

AAR-410 February 2, Subbase Equivalency Factors u Burns, C.D., R.H. Ledbetter, and R.W. Grau. u “Study of Behavior of Bituminous-Stabilized Pavement Layers,” Miscellaneous Paper S- 73-4, U.S. Army Engineer Waterways Experiment Station, Vicksburg, Mississipi, March u Bituminous stabilized base, asphalt base, bituminous stabilized subbase.

AAR-410 February 2, Subbase Equivalencies for 12-Wheel Traffic BLS stabilized layers replaced by MWHGL equivalent thicknesses

AAR-410 February 2, Subbase Equivalencies for 12-Wheel Traffic BLS stabilized layers replaced by MWHGL equivalent thicknesses

AAR-410 February 2, Alpha Factor Results - Discussion u Conversion of NAPTF structures gives better agreement with MWHGL test results. u This indicates that extra conservatism for subgrade protection has been built into the design procedure by increasing minimum thickness requirements for surface (5 in versus 3 in) and base (8 in versus 6 in) without reducing total thickness. u If 150/5320-6D is used to calibrate LEDFAA then LEDFAA is also conservative.

AAR-410 February 2, MWHGL Designs versus Current FAA CBR Designs u The MWHGL alpha factor curves give design thicknesses for structures with 3-in asphalt and 6-in base, and for material properties the same as the MWHGL test materials. u Thickness designs for other layer thicknesses and properties must be converted to MWHGL compatible structures to give the same level of subgrade protection x 33 in 1.15 x 28.7 in

AAR-410 February 2, Alpha Factor Results - Discussion u But, overconservative thicknesses for subgrade protection may provide other benefits for operation with heavy aircraft loads. u Safety factor for structural failure. u Compaction rutting in base and subbase materials. u Fatigue cracking of stabilized layers. u LEDFAA and FEDFAA are therefore being calibrated against -6D designs (5 and 8+ in), not MWHGL designs (3 and 6 in).

AAR-410 February 2, LEDFAA 1.3 Flexible Failure Model

AAR-410 February 2, North, 6-Wheel Track LFC1 LFC2 LFC3 LFC4 Subgrade CBR = 3.3

AAR-410 February 2, LFC1 Center Line, 6-Wheel Track LFC1 CBR = 4.3

February 2, CC-3 PHASE-2: LFC-1 CL TRAFFIC TESTS Pass No = 0 Pass No = 66 Pass No = 132 Pass No = 198 Pass No = 264 Pass No = 330

February 2, CC-3 PHASE-2 LFC-1 CL TRAFFIC TEST RESULTS

AAR-410 February 2, CC3-LFC1 Traffic Results Summary u A relatively small change in subgrade CBR can produce a very significant change in the magnitude and character of flexible pavement structural performance. u Very large deformations can occur at, say, 5 passes, even when the life to the failure criterion is as large as 100 passes. u This is the basis for the 240 coverage requirement in Engineering Brief No. 65, “Minimum Requirements to Widen Existing 150 ‑ Foot Wide Runways for Airbus A380 Operations.”