Design Methodology for Bonded Repair to Partial Through-Thickness Damage

Abstract

Partial through-thickness damage to metallic and composite structures, like those caused by corrosion damage of metals or foreign object impact to composites, can be repaired by adhesively bonding an insert and an external doubler. The design methodology for these types of repairs is based on a simplified analysis in which the insert is assumed to be bonded to the flat bottom of the cutout area. This report presents an investigation of the accuracy and limitations of the current design methodology using the finite element method. Improved design methods are also presented, including the optimum taper angle of the grindout and the required overlap length. Validity of the design methodology was assessed by comparison with experimental testing of repairs tapered at different angles.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2008
Accession Number
ADA494216

Entities

People

  • Chun H. Wang
  • Dina Pilalis

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Adhesives
  • Aircrafts
  • Composite Materials
  • Composite Structures
  • Engineering
  • Failure Mode And Effect Analysis
  • Finite Element Analysis
  • Materials
  • Mechanics
  • Modulus Of Elasticity
  • Payload
  • Shear Stresses
  • Standards
  • Thickness
  • Vehicles
  • Verification

Fields of Study

  • Materials science

Readers

  • Structural Health Monitoring of Composite Structures.