High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design

Suraj Ravindran; Subramani Sockalingam; Addis Kidane; Michael Sutton; Brian Justusson; Jenna Pang

doi:10.1007/978-3-319-95089-1_29

High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design

Suraj Ravindran, Subramani Sockalingam, Addis Kidane, Michael Sutton, Brian Justusson, Jenna Pang

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

3 Scopus citations

Abstract

Adhesively bonded carbon fiber-reinforced epoxy composite laminates are widely used in aerospace applications. During a high energy impact event, these laminates are often subjected to high strain rate loading. However, the influence of high strain rate loading on the response of these composite joints is not well understood. Computational finite element (FE) modeling and simulations are conducted to guide the design of high strain rate experiments. Two different experimental designs based on split Hopkinson bar were numerically modeled to simulate Mode I and Mode II types loading in the composite. In addition, the computational approach adopted in this study helps in understanding the high strain rate response of adhesively bonded composite joints subjected to nominally Mode I and Mode II loading. The modeling approach consists of a ply-level 3D FE model, a progressive damage constitutive model for the composite material behavior and a cohesive tie-break contact element for interlaminar delamination.

Original language	English (US)
Title of host publication	Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics
Editors	Jamie Kimberley, Leslie Elise Lamberson, Steven Mates
Publisher	Springer Science and Business Media, LLC
Pages	157-162
Number of pages	6
ISBN (Print)	9783319950884
DOIs	https://doi.org/10.1007/978-3-319-95089-1_29
State	Published - 2019
Externally published	Yes
Event	SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2018 - Greenville, United States Duration: Jun 4 2018 → Jun 7 2018

Publication series

Name	Conference Proceedings of the Society for Experimental Mechanics Series
ISSN (Print)	2191-5644
ISSN (Electronic)	2191-5652

Conference

Conference	SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2018
Country/Territory	United States
City	Greenville
Period	6/4/18 → 6/7/18

Bibliographical note

Publisher Copyright:
© The Society for Experimental Mechanics, Inc. 2019.

Keywords

Adhesive joint
Composite
Fracture
Mode I
Mode II

Publisher link

10.1007/978-3-319-95089-1_29

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Ravindran, S., Sockalingam, S., Kidane, A., Sutton, M., Justusson, B., & Pang, J. (2019). High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design. In J. Kimberley, L. E. Lamberson, & S. Mates (Eds.), Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics (pp. 157-162). (Conference Proceedings of the Society for Experimental Mechanics Series). Springer Science and Business Media, LLC. https://doi.org/10.1007/978-3-319-95089-1_29

High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design. / Ravindran, Suraj; Sockalingam, Subramani; Kidane, Addis et al.
Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics. ed. / Jamie Kimberley; Leslie Elise Lamberson; Steven Mates. Springer Science and Business Media, LLC, 2019. p. 157-162 (Conference Proceedings of the Society for Experimental Mechanics Series).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Ravindran, S, Sockalingam, S, Kidane, A, Sutton, M, Justusson, B & Pang, J 2019, High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design. in J Kimberley, LE Lamberson & S Mates (eds), Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics. Conference Proceedings of the Society for Experimental Mechanics Series, Springer Science and Business Media, LLC, pp. 157-162, SEM Annual Conference and Exposition on Experimental and Applied Mechanics, 2018, Greenville, United States, 6/4/18. https://doi.org/10.1007/978-3-319-95089-1_29

Ravindran S, Sockalingam S, Kidane A, Sutton M, Justusson B, Pang J. High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design. In Kimberley J, Lamberson LE, Mates S, editors, Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics. Springer Science and Business Media, LLC. 2019. p. 157-162. (Conference Proceedings of the Society for Experimental Mechanics Series). doi: 10.1007/978-3-319-95089-1_29

Ravindran, Suraj ; Sockalingam, Subramani ; Kidane, Addis et al. / High strain rate response of adhesively bonded fiber-reinforced composite joints : A computational study to guide experimental design. Dynamic Behavior of Materials, Volume 1 - Proceedings of the 2018 Annual Conference on Experimental and Applied Mechanics. editor / Jamie Kimberley ; Leslie Elise Lamberson ; Steven Mates. Springer Science and Business Media, LLC, 2019. pp. 157-162 (Conference Proceedings of the Society for Experimental Mechanics Series).

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AB - Adhesively bonded carbon fiber-reinforced epoxy composite laminates are widely used in aerospace applications. During a high energy impact event, these laminates are often subjected to high strain rate loading. However, the influence of high strain rate loading on the response of these composite joints is not well understood. Computational finite element (FE) modeling and simulations are conducted to guide the design of high strain rate experiments. Two different experimental designs based on split Hopkinson bar were numerically modeled to simulate Mode I and Mode II types loading in the composite. In addition, the computational approach adopted in this study helps in understanding the high strain rate response of adhesively bonded composite joints subjected to nominally Mode I and Mode II loading. The modeling approach consists of a ply-level 3D FE model, a progressive damage constitutive model for the composite material behavior and a cohesive tie-break contact element for interlaminar delamination.

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High strain rate response of adhesively bonded fiber-reinforced composite joints: A computational study to guide experimental design

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