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Syaiful Arif
SMK Negeri 2 Amuntai Hulu Sungai Utara Kal-Sel
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Journal : Otopro

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SIMULATION OF FATIGUE AND DEFORMATION OF CARBON FIBER DRONE PROPELLERS USING THE FINITE ELEMENT METHOD (FEM) Arif, Syaiful
Otopro Vol 21 No 2 May 2026
Publisher : Universitas Negeri Surabaya

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.26740/otopro.v21n2.p57-65

Abstract

This study analyses finite elements in the structural calculation of a drone propeller in carbon fiber with loads that represent live use. The output of this study evaluates the effect of load variations on deformation, stress distribution, and safety factors as key indicators of structural performance. A three-dimensional propeller model is developed based on the actual geometric configuration and analysed using the Finite Element Method (FEM). Several loadings are considered: a base load with a total mass of 3.6 kg, and two additional loading conditions with increasing masses of 0.5kg and 0.75kg. The applied loads are converted into equivalent forces distributed along the propeller blades to simulate realistic operating conditions. Simulations show that increasing the applied load causes a proportional increase in the maximum deformation and a significant reduction in the minimum safety factor. The maximum deformation increases from 14.933mm at the base load to 18.044mm at the highest load. The blade tip is consistently identified as a critical region, where the highest deformation and stress concentration occur due to bending-dominated behaviour. The safety factor ranges from 0.51341 to 0.42489 as the load increases, indicating a decrease in structural safety. Fatigue loading is mentioned, this study addresses fatigue qualitatively based on stress concentration and safety factor trends, as explicit S–N curve data, load cycle definitions, and mean stress corrections are not included. The results emphasize the importance of structural optimization and accurate material modelling to improve the reliability and durability of carbon fiber drone propellers under various load conditions.
Co-Authors Adin, Adin Ahmad Mujib, Ahmad alayuddin, Faqih Anabilla, Alifah Rahma Putri Andika, Mohamad Bagus Anggi Sofiana, Karisma Anggraini, Irma Novita Anugrah, Nazir Ultama Ardiansyah, Fakih Arif, Joni Arrasyid, Rizky Bambang Santoso Marsoem Bima Rizky Ananda Bohari Yusuf Budiono, Lukni Arif Diez Novitasari Evi Muafiah Faridi Faridi Febriansyah, Mochamad Duta Haickal Fenty Anggraeni, Erwinda Fenty Anggreeni, Erwinda Firdausi, Firna Nahwa Firmansyah, Heical Halomoan, Yosua Andhika Hanun Asrohah Juhaeri Kahlil Gibran, Muhammad Khalidiyah, Tuhfatul Koswara Lia Novita Mua’limin, Mua’limin Munzir Qadri Najiyah, Siti Firqo Nurdin, Ade Akhyar Nurul Ikhsan, Muhamad Pangestu, Dimas Dahlan Perkasa, Mustasyar Prasetia, Senata Adi Prayitno, Pungkas Prayoga, Bagus Purwadi Purwadi QOMARUZ ZAMAN Rafliansyah, Dhika Riana, Teguh Rustama, Daya Sabiqunassabiqun, Sabiqunassabiqun Santosa, Yogi Saputra, Aswin Caesar Sari, Shilvi Nofita Sunarto Sunarto Syahwati, Fitriana Syaiful Arif Ubai Dillah Velayati, Jihan Maghfiroh Wahid Hasim Wibowo, Reson WIDYA PH, KHAIRINA Yohan Yudhaningrum, Lupi Zaki, Faisal