On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates

Xiaodong Xu; Aakash Paul; Michael Wisnom

On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates

Xiaodong Xu, Aakash Paul, Michael Wisnom

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

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Abstract

Trans-laminar fracture toughness was measured in a series of centre-notched quasi-isotropic IM7/8552 carbon/epoxy laminates with scaled specimens of thickness between 2 and 8 mm. The aim was to find out if there is a transition laminate thickness at which there is a change in fracture toughness. No dependency on specimen thickness was found for specimens with 12.7 mm and 25.4 mm centre notches. There is a discrepancy compared with the findings of the previous literature. The potential causes are discussed.

Original language	English
Title of host publication	Proceedings of the American Society for Composites 2016
Subtitle of host publication	Thirty-First Technical Conference on Composite Materials
Editors	Barry D Davidson, James G Ratcliffe, Michael W Czabaj
Publisher	DEStech Publications, Inc.
Number of pages	6
ISBN (Electronic)	9781605953168
Publication status	Published - Oct 2016
Event	31st Technical Conference of the American Society for Composites: ASC 2016 - Williamsburg Lodge, Williamsburg , United States Duration: 19 Sept 2016 → 21 Sept 2016

Conference

Conference	31st Technical Conference of the American Society for Composites
Country/Territory	United States
City	Williamsburg
Period	19/09/16 → 21/09/16

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This is the author accepted manuscript (AAM). The final published version (version of record) is available via DEStech at www.destechpub.com/product/proceedings-american-society-composites-thirty-first-technical-conference-composite-materials/. Please refer to any applicable terms of use of the publisher.
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Xu, Xiaodong ; Paul, Aakash ; Wisnom, Michael. / On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates. Proceedings of the American Society for Composites 2016: Thirty-First Technical Conference on Composite Materials. editor / Barry D Davidson ; James G Ratcliffe ; Michael W Czabaj. DEStech Publications, Inc., 2016.

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title = "On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates",

abstract = "Trans-laminar fracture toughness was measured in a series of centre-notched quasi-isotropic IM7/8552 carbon/epoxy laminates with scaled specimens of thickness between 2 and 8 mm. The aim was to find out if there is a transition laminate thickness at which there is a change in fracture toughness. No dependency on specimen thickness was found for specimens with 12.7 mm and 25.4 mm centre notches. There is a discrepancy compared with the findings of the previous literature. The potential causes are discussed.",

author = "Xiaodong Xu and Aakash Paul and Michael Wisnom",

year = "2016",

month = oct,

language = "English",

editor = "Davidson, {Barry D} and Ratcliffe, {James G} and Czabaj, {Michael W}",

booktitle = "Proceedings of the American Society for Composites 2016",

publisher = "DEStech Publications, Inc.",

note = " 31st Technical Conference of the American Society for Composites : ASC 2016 ; Conference date: 19-09-2016 Through 21-09-2016",

}

Xu, X, Paul, A & Wisnom, M 2016, On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates. in BD Davidson, JG Ratcliffe & MW Czabaj (eds), Proceedings of the American Society for Composites 2016: Thirty-First Technical Conference on Composite Materials. DEStech Publications, Inc., 31st Technical Conference of the American Society for Composites, Williamsburg , United States, 19/09/16.

On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates. / Xu, Xiaodong; Paul, Aakash; Wisnom, Michael.
Proceedings of the American Society for Composites 2016: Thirty-First Technical Conference on Composite Materials. ed. / Barry D Davidson; James G Ratcliffe; Michael W Czabaj. DEStech Publications, Inc., 2016.

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

TY - GEN

T1 - On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates

AU - Xu, Xiaodong

AU - Paul, Aakash

AU - Wisnom, Michael

PY - 2016/10

Y1 - 2016/10

N2 - Trans-laminar fracture toughness was measured in a series of centre-notched quasi-isotropic IM7/8552 carbon/epoxy laminates with scaled specimens of thickness between 2 and 8 mm. The aim was to find out if there is a transition laminate thickness at which there is a change in fracture toughness. No dependency on specimen thickness was found for specimens with 12.7 mm and 25.4 mm centre notches. There is a discrepancy compared with the findings of the previous literature. The potential causes are discussed.

AB - Trans-laminar fracture toughness was measured in a series of centre-notched quasi-isotropic IM7/8552 carbon/epoxy laminates with scaled specimens of thickness between 2 and 8 mm. The aim was to find out if there is a transition laminate thickness at which there is a change in fracture toughness. No dependency on specimen thickness was found for specimens with 12.7 mm and 25.4 mm centre notches. There is a discrepancy compared with the findings of the previous literature. The potential causes are discussed.

M3 - Conference Contribution (Conference Proceeding)

BT - Proceedings of the American Society for Composites 2016

A2 - Davidson, Barry D

A2 - Ratcliffe, James G

A2 - Czabaj, Michael W

PB - DEStech Publications, Inc.

T2 - 31st Technical Conference of the American Society for Composites

Y2 - 19 September 2016 through 21 September 2016

ER -

On the Relationship between Fracture Toughness and Specimen Thickness for Quasi-isotropic Carbon/Epoxy Laminates

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