Design parameters and associated quantitative damage analyses of an asphalt concrete airfield runway

•Design and numerical damage analyses of an airfield runway pavement are carried out.•Materials, mechanical behavior models and aircraft are defined to pavement design.•Linear elastic and viscoelastic numerical analyses are the main evaluation scopes.•Viscoelastic analyses provide more discriminatin...

Full description

Saved in:
Bibliographic Details
Published in:Construction & building materials Vol. 262; p. 120809
Main Authors: Barra, Breno, Neckel, Glauciano, Momm, Leto, Guerrero, Yader, Mikowski, Alexandre, Melo, João Victor Staub de, Nguyen, Mai-Lan, Hughes, Gary B.
Format: Journal Article
Language:English
Published: Elsevier Ltd 30-11-2020
Elsevier
Subjects:
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary:•Design and numerical damage analyses of an airfield runway pavement are carried out.•Materials, mechanical behavior models and aircraft are defined to pavement design.•Linear elastic and viscoelastic numerical analyses are the main evaluation scopes.•Viscoelastic analyses provide more discriminating assessment of damage phenomena.•Landing gear geometric configuration plays decisive role on damage propagation. Design parameters and evaluation of associated mechanical behavior of an airfield runway asphalt concrete pavement structure is reported. French aeronautical design methodology was taken as reference. Field and laboratory procedures were employed to determine constituent materials of the designed structure. Stationary linear elastic and dynamic viscoelastic numerical damage analyses were developed and compared, using computerized tools based on 3D Finite Element Methods. Results indicate that viscoelastic analyses provide more discriminating assessment of damage phenomena along the depth of pavement layers, and that landing gear geometric characteristics are more diagnostic than aircraft gross weight for cumulative damage propagation.
ISSN:0950-0618
1879-0526
DOI:10.1016/j.conbuildmat.2020.120809