Research Article

Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate

Volume: 14 Number: 3 September 30, 2025

Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate

Abstract

This study investigated the dynamic properties of a spherical sandwich composite structure made of carbon fiber face sheets and a Nomex honeycomb core. The structure was produced using the hand lay-up method. The results from Experimental Modal Analysis (EMA) and the numerical model created in ANSYS showed high consistency. The natural frequency difference was only 0.73% for the second mode, with the largest discrepancy of 6.5% was observed in the first mode. These differences are thought to be related to structural variations from the manufacturing process, such as resin distribution, carbon fiber fabric stacking, and air voids and the experimental challenges such as double hit errors, measurement resolutions related to force sensor and accelerometer and environmental noise. The vibration damping capability of the sandwich structure was investigated. Some modes exhibited high damping, while others had relatively lower values. The highest and the lowest damping ratios were obtained as 0.83% for the third mode and 0.23% for the fourth mode. A numerical equivalent model of the structure was created in ANSYS to determine its natural frequencies and vibration modes, confirming its effectiveness in modeling complex structures.

Keywords

References

  1. Pach, J., Wroblewski, R., Muszynski, B. Comparative Analysis of Sandwich Composites with Balsa, Rohacell, and Nomex Cores for Aerospace Applications, Materials, 2025, 18, 1126.
  2. Sahib, M.M., Kovács, G. Using Artificial Neural Networks to Predict the Bending Behavior of Composite Sandwich Structures, Polymers 2025, 17, 337.
  3. Çelik, M., Güden, M., Sarıkaya, M., Tasdemirci¸ A., Genç, C., Ersoy, K., Serin, O. The impact response of a Nomex® honeycomb core/E-glass/epoxy composite sandwich structure to increasing velocities: Experimental and numerical analysis, Composite Structures 320 (2023) 117205.
  4. Sadiq, S.E., Bakhy, S.H., Jweeg, M.J. Optimum Vibration Characteristics for Honey Comb Sandwich Panel Used in Aircraft Structure, Journal of Engineering Science and Technology, Vol. 16, No. 2 (2021) 1463 – 1479.
  5. Ejaz, H., Khalid, S., Saeed, M.B., Nadeem, A. Flexural and impact response of sandwich panels with Nomex honeycomb core and hybrid fiber composite skins, Journal of Sandwich Structures & Materials, 2025, Vol. 27(1) 32–50.
  6. Naufal, A.M., Prabowo, A.R., Muttaqie, T., Hidayat, A., Purwono J., Adiputra, R., Akbar, H.I., Smaradhana, D.F. Characterization of sandwich materials – Nomex-Aramid carbon fiber performances under mechanical loadings: Nonlinear FE and convergence studies, Reviews on Advanced Materials Science 2024; 63: 20230177.
  7. Chen, X., Fan, H. Flexible forming mechanism of curved sandwich shell with flexible honeycombs and twill carbon fiber fabrics, Composite Structures 354 (2025) 118779.
  8. Tran, T.T., Pham, Q.H., Nguyen-Thoi, T., Tran, T. Van (2020). Dynamic Analysis of Sandwich Auxetic Honeycomb Plates Subjected to Moving Oscillator Load on Elastic Foundation, Advances in Materials Science and Engineering, 2020.

Details

Primary Language

English

Subjects

Dynamics, Vibration and Vibration Control, Machine Theory and Dynamics

Journal Section

Research Article

Publication Date

September 30, 2025

Submission Date

July 17, 2025

Acceptance Date

September 27, 2025

Published in Issue

Year 2025 Volume: 14 Number: 3

APA
Yiğid, O., & Şen, M. (2025). Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi, 14(3), 1961-1979. https://doi.org/10.17798/bitlisfen.1745184
AMA
1.Yiğid O, Şen M. Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi. 2025;14(3):1961-1979. doi:10.17798/bitlisfen.1745184
Chicago
Yiğid, Osman, and Murat Şen. 2025. “Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate”. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi 14 (3): 1961-79. https://doi.org/10.17798/bitlisfen.1745184.
EndNote
Yiğid O, Şen M (September 1, 2025) Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi 14 3 1961–1979.
IEEE
[1]O. Yiğid and M. Şen, “Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate”, Bitlis Eren Üniversitesi Fen Bilimleri Dergisi, vol. 14, no. 3, pp. 1961–1979, Sept. 2025, doi: 10.17798/bitlisfen.1745184.
ISNAD
Yiğid, Osman - Şen, Murat. “Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate”. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi 14/3 (September 1, 2025): 1961-1979. https://doi.org/10.17798/bitlisfen.1745184.
JAMA
1.Yiğid O, Şen M. Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi. 2025;14:1961–1979.
MLA
Yiğid, Osman, and Murat Şen. “Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate”. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi, vol. 14, no. 3, Sept. 2025, pp. 1961-79, doi:10.17798/bitlisfen.1745184.
Vancouver
1.Osman Yiğid, Murat Şen. Experimental and Numerical Modal Analysis of Nomex Honeycomb Core Composite Sandwich Spherical Plate. Bitlis Eren Üniversitesi Fen Bilimleri Dergisi. 2025 Sep. 1;14(3):1961-79. doi:10.17798/bitlisfen.1745184

Cited By

Bitlis Eren University

Journal of Science Editor

Bitlis Eren University Graduate Institute

Bes Minare Mah. Ahmet Eren Bulvari, Merkez Kampus, 13000 BITLIS

E-mail: fbe@beu.edu.tr