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All Journal Prosiding SNATIF Jurnal Penelitian Pendidikan IPA (JPPIPA) International Conferences SDGs 2030 Challenges and Solutions JURNAL INSTEK (Informatika Sains dan Teknologi) Jurnal Teknik Elektro dan Komputer TRIAC TELKA - Telekomunikasi, Elektronika, Komputasi dan Kontrol INAJEEE (Indonesian Journal of Electrical and Electronics Engineering) JTEIN: Jurnal Teknik Elektro Indonesia Jurnal Telkommil Jurnal Elkasista Journal Of World Science Journal of Innovation Research and Knowledge Eduvest - Journal of Universal Studies Jurnal Penelitian dan Pengkajian Ilmiah
Nur Rachman Supadmana Muda
Departement Of Telecomunication Of Poltekad College, Batu
Aerospace Engineering Agriculture, Biological Sciences & Forestry Humanities Biochemistry, Genetics & Molecular Biology Chemical Engineering, Chemistry & Bioengineering Chemistry Computer Science & IT Control & Systems Engineering Economics, Econometrics & Finance Education Electrical & Electronics Engineering Energy Engineering Environmental Science Health Professions Law, Crime, Criminology & Criminal Justice Materials Science & Nanotechnology Neuroscience Physics Public Health Social Sciences

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Journal : Jurnal Penelitian Pendidikan IPA (JPPIPA)

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Analysis of Stable Flight of Poltekad Eagle Drone Using ANSYS Method Muda, Nur Rachman Supadmana; Gumilar, Nugraha; Wiyanto, Suko; Kholid, Fajar
Jurnal Penelitian Pendidikan IPA Vol 10 No 11 (2024): November
Publisher : Postgraduate, University of Mataram

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.29303/jppipa.v10i11.8732

Abstract

The purpose of this study was to analyze the movement of the wings of a self-made eagle drone using the ANSYS method. The drone analyzed for the wing type moves to fly by being thrown when the brushless motor throttle moves the flapping of the wings at maximum rotation. The aerodynamic model used for data analysis in this paper is optimized to determine and improve the operational performance of the wings of eagle drones, especially in terms of stability and flight time. These two aspects are very important to determine the efficiency of drone performance. The method used for simulation analysis uses ANSYS 13. In the next step, the numerical results will be compared with the results during the experimental flight process. The conclusion of this study presents the main results of the simulation, namely numerical magnitude, main flight coefficient and flight time that affect stable flight efficiency.
Co-Authors Abdul Rasyid Aswansyah Anggraini Puspita Sari Aries Boedi Setiawan Aswansyah, Abdul Rasyid Dekki Widiatmoko Fadilah, M.Faisal Faranadila, Bilqis Farandila, Bilqis GINANJAR, GINANJAR Gumilar, Nugraha Hana, Dinar Herkariawan, Chandra I.N.G.Wardana I.N.G.Wardana Juanda Rahimatullah Kholid, Fajar krisna krisnawati wati KUNCORO, EKO Lilis Yuliati M. M. Hudha MHD Iqbal Fahmi Minggu, Desyderius Muhamad Yusuf Imani Nabila, Dinar Safa Nachrowie Nachrowie Nachrowie, Nachrowie Nadhif Misbachul Hidayat Nurkholis Hamidi Prisca Chorina Putra, Yossy Tamara sa'id a'inul yaqin Safanabila, Dinar Salman Salman Sridaryono, Aguk Transallia, Azizia Putri Wellyanto, Mochammad Alif Wisesha, Pandhu Purba Wiyanto, Suko Yaqin, Sa'id A'inul Zani Akbari