High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods

Mustafa Bilgin; Fatih Usta; Halit S. Turkmen; Ugur Yolum

doi:10.1109/RAST57548.2023.10197951

High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods

Mustafa Bilgin, Fatih Usta, Halit S. Turkmen, Ugur Yolum

Uçak Mühendisliği Bölümü

Araştırma sonucu: ???type-name??? › Konferans katkısı › bilirkişi

Özet

The impact response of honeycomb sandwich structures under high-velocity impact is greatly significant because of their wide usage in aviation. This paper presents an experimental and numerical investigation of the impact responses of the sandwich panel with a Nomex honeycomb core and composite face sheets. Numerical studies are performed by using ABAQUS/Explicit. The experimental studies are fulfilled as sandwich panel manufacturing and high-velocity impact testing. The numerical model which was verified can observe sandwich panel deformation on high-velocity impact, sandwich panel ballistic limit, and the energy absorption rate of sandwich panel structures (core, face sheets). Results show that the ballistic limits of the sandwich panel decrease with increasing impact velocity, and most of the energy is absorbed by the core of the sandwich structure compared to the face sheets.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
ISBN (Elektronik)	9798350323023
DOI'lar	https://doi.org/10.1109/RAST57548.2023.10197951
Yayın durumu	Yayınlandı - 2023
Etkinlik	10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 - Istanbul, Turkey Süre: 7 Haz 2023 → 9 Haz 2023

Yayın serisi

Adı	Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023
Ülke/Bölge	Turkey
Şehir	Istanbul
Periyot	7/06/23 → 9/06/23

Bibliyografik not

Publisher Copyright:
© 2023 IEEE.

Finansman

ACKNOWLEDGMENT Support for this work has been provided by the Turkish Aerospace Industries, INC under Project Number 2021-BAP-14.

Finansörler	Finansör numarası
Türk Havacılık ve Uzay Sanayii	2021-BAP-14

Belgeye Erişim

10.1109/RAST57548.2023.10197951

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Bilgin, M., Usta, F., Turkmen, H. S., & Yolum, U. (2023). High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods. In Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 (Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST57548.2023.10197951

Bilgin, Mustafa ; Usta, Fatih ; Turkmen, Halit S. et al. / High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods. Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023. Institute of Electrical and Electronics Engineers Inc., 2023. (Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023).

@inproceedings{0f0f45c0119f42fbb2f4a907424bc977,

title = "High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods",

abstract = "The impact response of honeycomb sandwich structures under high-velocity impact is greatly significant because of their wide usage in aviation. This paper presents an experimental and numerical investigation of the impact responses of the sandwich panel with a Nomex honeycomb core and composite face sheets. Numerical studies are performed by using ABAQUS/Explicit. The experimental studies are fulfilled as sandwich panel manufacturing and high-velocity impact testing. The numerical model which was verified can observe sandwich panel deformation on high-velocity impact, sandwich panel ballistic limit, and the energy absorption rate of sandwich panel structures (core, face sheets). Results show that the ballistic limits of the sandwich panel decrease with increasing impact velocity, and most of the energy is absorbed by the core of the sandwich structure compared to the face sheets.",

keywords = "ballistic limit, energy absorption, high-velocity impact, sandwich panel",

author = "Mustafa Bilgin and Fatih Usta and Turkmen, {Halit S.} and Ugur Yolum",

note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 ; Conference date: 07-06-2023 Through 09-06-2023",

year = "2023",

doi = "10.1109/RAST57548.2023.10197951",

language = "English",

series = "Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

booktitle = "Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023",

address = "United States",

}

Bilgin, M, Usta, F, Turkmen, HS & Yolum, U 2023, High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods. in Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023. Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, Institute of Electrical and Electronics Engineers Inc., 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023, Istanbul, Turkey, 7/06/23. https://doi.org/10.1109/RAST57548.2023.10197951

High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods. / Bilgin, Mustafa; Usta, Fatih; Turkmen, Halit S. et al.
Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023. Institute of Electrical and Electronics Engineers Inc., 2023. (Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023).

Araştırma sonucu: ???type-name??? › Konferans katkısı › bilirkişi

TY - GEN

T1 - High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods

AU - Bilgin, Mustafa

AU - Usta, Fatih

AU - Turkmen, Halit S.

AU - Yolum, Ugur

PY - 2023

Y1 - 2023

N2 - The impact response of honeycomb sandwich structures under high-velocity impact is greatly significant because of their wide usage in aviation. This paper presents an experimental and numerical investigation of the impact responses of the sandwich panel with a Nomex honeycomb core and composite face sheets. Numerical studies are performed by using ABAQUS/Explicit. The experimental studies are fulfilled as sandwich panel manufacturing and high-velocity impact testing. The numerical model which was verified can observe sandwich panel deformation on high-velocity impact, sandwich panel ballistic limit, and the energy absorption rate of sandwich panel structures (core, face sheets). Results show that the ballistic limits of the sandwich panel decrease with increasing impact velocity, and most of the energy is absorbed by the core of the sandwich structure compared to the face sheets.

AB - The impact response of honeycomb sandwich structures under high-velocity impact is greatly significant because of their wide usage in aviation. This paper presents an experimental and numerical investigation of the impact responses of the sandwich panel with a Nomex honeycomb core and composite face sheets. Numerical studies are performed by using ABAQUS/Explicit. The experimental studies are fulfilled as sandwich panel manufacturing and high-velocity impact testing. The numerical model which was verified can observe sandwich panel deformation on high-velocity impact, sandwich panel ballistic limit, and the energy absorption rate of sandwich panel structures (core, face sheets). Results show that the ballistic limits of the sandwich panel decrease with increasing impact velocity, and most of the energy is absorbed by the core of the sandwich structure compared to the face sheets.

KW - ballistic limit

KW - energy absorption

KW - high-velocity impact

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T3 - Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023

BT - Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023

PB - Institute of Electrical and Electronics Engineers Inc.

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Bilgin M, Usta F, Turkmen HS, Yolum U. High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods. In Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023. Institute of Electrical and Electronics Engineers Inc. 2023. (Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023). doi: 10.1109/RAST57548.2023.10197951

High-velocity Impact Responses of Composite Sandwich Panels with Honeycomb Core by Using Experimental and Numerical Methods

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