Analysis of load-induced strains in a hot mix asphalt perpetual pavement : final report, April 2009.
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Analysis of load-induced strains in a hot mix asphalt perpetual pavement : final report, April 2009.

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  • English

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      Final report; June 2005-Apr. 2009.
    • Abstract:
      This report presents the findings of a research study conducted to investigate the structural performance of a 275 mm hot

      mix asphalt perpetual pavement constructed as part of the WIM bypass lane at the Kenosha Safety & Weigh Station

      Facility. Two separate test sections were constructed using variable binder types and in-place air voids. Asphalt strain

      sensors were fabricated at Marquette University and installed during the construction of the HMA pavement. Sensors were

      positioned within the outer wheel path and located at the bottom of the 275 mm HMA pavement and at the interface

      between the lower layers at a depth of approximately 175mm from the surface. Strain sensors were oriented in both the

      transverse and longitudinal directions. A total of 16 strain sensors were installed during construction. Of these, only three

      survived to provide strain data under traffic loadings.

      Deflection data obtained from FWD testing was used as comparative measures to strain measurements obtained during

      testing and to estimate the combined dynamic HMA layer moduli at the time of testing and to develop monthly trends of

      dynamic HMA layer moduli as a function of the expected mean monthly mid-depth pavement temperature. A comparative

      analysis of measured strains to those predicted from FWD measurements provided generally good agreement. A

      mechanistic appraisal of the constructed test sections was completed using the outputs of the EVERSTRESS pavement

      analysis program. This analysis computed the expected monthly damage induced by the application of 521,000 monthly

      ESAL loadings. The results of the mechanistic appraisal indicate the expected service life to 50% bottom-up fatigue

      cracking is in excess of 90 years for sections with air voids of 4% within the lower layers. If the air void content increases

      to 5% - 6% in the lower layers, the expected fatigue life may be significantly reduced to between 13 – 32 years.

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