Damage tolerance coupon sizing of composite stiffened panels under impact

Hamid Dalir

doi:10.1109/ICMAE.2016.7549510

Damage tolerance coupon sizing of composite stiffened panels under impact

Hamid Dalir

Department of Mechanical & Aerospace Engineering

Research output: Chapter in Book/Entry/Poem › Conference contribution

Abstract

The design of aircraft composite stiffened structures subjected to dynamic and impact loadings requires several experimental testing scenarios on the full-size structure. The present paper deals with investigating the feasibility of the use of sub-size test specimens under vertical and lateral impacts on the stiffener free flange based on finite element (FE) models. Simulations were performed on sub-size specimens carefully extracted from the full-size (26.4 × 48.4 × 2.4 in³) impact test panels. The main required specifications of an in-house falling weight impact tester were also determined, discussing the required fixture/jig configuration.

Original language	English (US)
Title of host publication	Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	68-72
Number of pages	5
ISBN (Electronic)	9781467388290
DOIs	https://doi.org/10.1109/ICMAE.2016.7549510
State	Published - Aug 23 2016
Event	7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016 - London, United Kingdom Duration: Jul 18 2016 → Jul 20 2016

Publication series

Name	Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016

Other

Other	7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016
Country/Territory	United Kingdom
City	London
Period	7/18/16 → 7/20/16

Keywords

composite stiffened panel
finite element analysis
fixture/jig
impact testing

ASJC Scopus subject areas

Aerospace Engineering
Mechanical Engineering

Access to Document

10.1109/ICMAE.2016.7549510

Cite this

Dalir, H. (2016). Damage tolerance coupon sizing of composite stiffened panels under impact. In Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016 (pp. 68-72). Article 7549510 (Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMAE.2016.7549510

Damage tolerance coupon sizing of composite stiffened panels under impact. / Dalir, Hamid.
Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016. Institute of Electrical and Electronics Engineers Inc., 2016. p. 68-72 7549510 (Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016).

Research output: Chapter in Book/Entry/Poem › Conference contribution

Dalir, H 2016, Damage tolerance coupon sizing of composite stiffened panels under impact. in Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016., 7549510, Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016, Institute of Electrical and Electronics Engineers Inc., pp. 68-72, 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016, London, United Kingdom, 7/18/16. https://doi.org/10.1109/ICMAE.2016.7549510

Dalir H. Damage tolerance coupon sizing of composite stiffened panels under impact. In Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016. Institute of Electrical and Electronics Engineers Inc. 2016. p. 68-72. 7549510. (Proceedings of 2016 7th International Conference on Mechanical and Aerospace Engineering, ICMAE 2016). doi: 10.1109/ICMAE.2016.7549510

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Damage tolerance coupon sizing of composite stiffened panels under impact

Abstract

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Keywords

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