Experimental Verification of Dynamic Properties of a Hollow Aluminum Beam-Reference-Cited by-同舟云学术

Experimental Verification of Dynamic Properties of a Hollow Aluminum Beam

Published:2023-12-27 Issue:3 Volume:5 Page:149-162
ISSN:2667-7814
Container-title:ALKÜ Fen Bilimleri Dergisi
language:
Short-container-title:

Author:

BİLİR Mert¹^ORCID,KARAKAŞ Muhsin¹^ORCID,OKTAV Akın¹^ORCID,ÖZDEMİR Emre¹^ORCID,SAVİ Ahmet Selim¹^ORCID,SEVİNÇ Fatih¹^ORCID,TÜRKAN Hasan Ali¹^ORCID

Affiliation:

1. ALANYA ALAADDİN KEYKUBAT ÜNİVERSİTESİ

Abstract

In this study, analytical and computational analyses are performed to determine the dynamic properties of an aluminum hollow beam and an experimental analysis is also performed. The experimental model is taken as a reference model and the computational model is updated accordingly using model updating tools. The damping behavior inherent in all physical structures is measured experimentally. According to the results of the cross-correlation modal assurance criterion, the experimental and computational results match well. The average error between the computational and experimental results for the first five damped natural frequency values is 1.5%.

Funder

TÜBİTAK

Publisher

ALKU Fen Bilimleri Dergisi, Alanya Alaaddin Keykubat University

Subject

General Earth and Planetary Sciences

Reference22 articles.

1. [1] Zannon, M. (2014). Free vibration of thin film cantilever beam. International Journal of Engineering and Technical Research (IJETR), 2, 304-314.

2. [2] Piranda, J., Corn, S., Bouhaddi, N., Stawicki, C., Van Herpe, F., & Cudney, H. H. (1998, February). Determination of equivalent beam properties for hollow girders typically used in the automotive industry. In Society for Experimental Mechanics, Inc, 16 th International Modal Analysis Conference. (Vol. 2, pp. 1227-1232).

3. [3] Machhan, R. A., & Könke, C. (2021). Investigation of different types of damping effects for automotive components–preliminary work. Materials Today: Proceedings, 46, 9659-9666.

4. [4] Demirtaş, A., & Bayraktar, M. (2019). Free vibration analysis of an aircraft wing by considering as a cantilever beam. Selçuk Üniversitesi Mühendislik, Bilim Ve Teknoloji Dergisi, 7(1), 12-21.

5. [5]Chaphalkar, S. P., Khetre, S. N., & Meshram, A. M. (2015). Modal analysis of cantilever beam structure using finite element analysis and experimental analysis. American Journal of Engineering Research, 4(10), 178-185.