A finite element study of fatigue crack propagation in single lap bonded joints with process-induced disbond

Yiding Liu, Stuart Lemanski, Xiang Zhang, David Ayres, Hamed Yazdani Nezhad

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2 Citations (Scopus)

Abstract

This paper presents a method for predicting fatigue crack propagation in single lap adhesively bonded composite joints with an initial full-width pre-existing disbond using finite element analysis and numerical integration of the fatigue crack growth rate law. Fatigue tests were conducted on the single lap joints to monitor crack lengths from four runout corners. A novel in-situ crack growth measurement technique has been developed using red ink injection through a needle nozzle through the interface over the lap in order to identify the crack propagation profile during tensile-tensile fatigue loading. The crack growth was modelled using a fracture mechanics criterion under quasi-static conditions in finite element analysis. Two model assumptions were made considering the crack length from one runout end alone, and under the influence of crack length from the other runout end occurring due to fatigue load. The crack growth rate law was determined experimentally using the standard double cantilever beam (DCB), mixed mode bending (MMB) and end notch flexure (ENF) specimens. The numerical models based on the crack propagation in the adherend-adhesive interface and crack growth rate data from mixed mode tests, allowed for predicting the lower and upper bounds of the fatigue crack growth rate of the single lap joints, observed during fatigue tests with good accuracy.
Original languageEnglish
Pages (from-to)164-172
Number of pages7
JournalInternational Journal of Adhesion and Adhesives
Volume87
Early online date9 Oct 2018
DOIs
Publication statusPublished - Dec 2018

Fingerprint

Fatigue crack propagation
Crack propagation
Fatigue of materials
Cracks
Finite element method
Cantilever beams
Ink
Fracture mechanics
Needles
Numerical models
Nozzles
Adhesives
Composite materials

Keywords

  • single lap joints
  • adhesive bond
  • finite element analysis
  • fatigue crack growth rate
  • fatigue life prediction

Cite this

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title = "A finite element study of fatigue crack propagation in single lap bonded joints with process-induced disbond",
abstract = "This paper presents a method for predicting fatigue crack propagation in single lap adhesively bonded composite joints with an initial full-width pre-existing disbond using finite element analysis and numerical integration of the fatigue crack growth rate law. Fatigue tests were conducted on the single lap joints to monitor crack lengths from four runout corners. A novel in-situ crack growth measurement technique has been developed using red ink injection through a needle nozzle through the interface over the lap in order to identify the crack propagation profile during tensile-tensile fatigue loading. The crack growth was modelled using a fracture mechanics criterion under quasi-static conditions in finite element analysis. Two model assumptions were made considering the crack length from one runout end alone, and under the influence of crack length from the other runout end occurring due to fatigue load. The crack growth rate law was determined experimentally using the standard double cantilever beam (DCB), mixed mode bending (MMB) and end notch flexure (ENF) specimens. The numerical models based on the crack propagation in the adherend-adhesive interface and crack growth rate data from mixed mode tests, allowed for predicting the lower and upper bounds of the fatigue crack growth rate of the single lap joints, observed during fatigue tests with good accuracy.",
keywords = "single lap joints, adhesive bond, finite element analysis, fatigue crack growth rate, fatigue life prediction",
author = "Yiding Liu and Stuart Lemanski and Xiang Zhang and David Ayres and {Yazdani Nezhad}, Hamed",
year = "2018",
month = "12",
doi = "10.1016/j.ijadhadh.2018.10.005",
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T1 - A finite element study of fatigue crack propagation in single lap bonded joints with process-induced disbond

AU - Liu, Yiding

AU - Lemanski, Stuart

AU - Zhang, Xiang

AU - Ayres, David

AU - Yazdani Nezhad, Hamed

PY - 2018/12

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N2 - This paper presents a method for predicting fatigue crack propagation in single lap adhesively bonded composite joints with an initial full-width pre-existing disbond using finite element analysis and numerical integration of the fatigue crack growth rate law. Fatigue tests were conducted on the single lap joints to monitor crack lengths from four runout corners. A novel in-situ crack growth measurement technique has been developed using red ink injection through a needle nozzle through the interface over the lap in order to identify the crack propagation profile during tensile-tensile fatigue loading. The crack growth was modelled using a fracture mechanics criterion under quasi-static conditions in finite element analysis. Two model assumptions were made considering the crack length from one runout end alone, and under the influence of crack length from the other runout end occurring due to fatigue load. The crack growth rate law was determined experimentally using the standard double cantilever beam (DCB), mixed mode bending (MMB) and end notch flexure (ENF) specimens. The numerical models based on the crack propagation in the adherend-adhesive interface and crack growth rate data from mixed mode tests, allowed for predicting the lower and upper bounds of the fatigue crack growth rate of the single lap joints, observed during fatigue tests with good accuracy.

AB - This paper presents a method for predicting fatigue crack propagation in single lap adhesively bonded composite joints with an initial full-width pre-existing disbond using finite element analysis and numerical integration of the fatigue crack growth rate law. Fatigue tests were conducted on the single lap joints to monitor crack lengths from four runout corners. A novel in-situ crack growth measurement technique has been developed using red ink injection through a needle nozzle through the interface over the lap in order to identify the crack propagation profile during tensile-tensile fatigue loading. The crack growth was modelled using a fracture mechanics criterion under quasi-static conditions in finite element analysis. Two model assumptions were made considering the crack length from one runout end alone, and under the influence of crack length from the other runout end occurring due to fatigue load. The crack growth rate law was determined experimentally using the standard double cantilever beam (DCB), mixed mode bending (MMB) and end notch flexure (ENF) specimens. The numerical models based on the crack propagation in the adherend-adhesive interface and crack growth rate data from mixed mode tests, allowed for predicting the lower and upper bounds of the fatigue crack growth rate of the single lap joints, observed during fatigue tests with good accuracy.

KW - single lap joints

KW - adhesive bond

KW - finite element analysis

KW - fatigue crack growth rate

KW - fatigue life prediction

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JF - International Journal of Adhesion and Adhesives

SN - 0143-7496

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