PENGARUH PARAMETER VARIASI ASPEK RASIO PADA ANALISIS CFD AERODINAMIKA AIRFOIL NACA 0012
DOI:
https://doi.org/10.31949/jensitec.v10i01.5525Abstrak
Indonesia, as the world's largest archipelagic country, benefits from its unique geographical conditions, making airplanes the most suitable mode of transportation. This is evident from the increasing number of airlines, a notable development in the aviation field, particularly in military aviation, is the advancement of drones or Unmanned Aerial Vehicles (UAVs). In recent years, there has been rapid technological progress in fixed-wing UAV technology. UAVs are unmanned aircraft that can be remotely controlled by pilots or capable of autonomous flight using aerodynamic principles to generate lift. Fixed-wing UAVs have wings with a fixed configuration. Unmanned aircraft offer several advantages over manned aircraft, including extended airborne endurance with efficient fuel consumption, categorized as Medium Altitude Endurance UAVs (MALE UAVs). These UAVs optimize the Lift-to-Drag ratio (CL/CD) to improve their performance. Currently, unmanned aircraft are being extensively developed for various purposes, such as exploration, reconnaissance, mining, military applications, competitions, and more.
Kata Kunci:
UAV, Aspect Ratio, Lift to Drag Ratio, AirfoilUnduhan
Referensi
A. Saputra, H. E. Priyono, I. Hidayat, L. Iryani, and D. M. Gunara, “MODIFIKASI AIRFOIL SAYAP PESAWAT CONCEPTUAL TRANSPORT RM-001,” Bandung, 2016. Accessed: Dec. 19, 2022. [Online]. Available: https://jurnal.unnur.ac.id/index.php/indept/article/view/174/145
J. Cornel, R. Siahaan, A. Munawir, Z. Husin, and J. T. Mesin, “ANALISIS GAYA DORONG (THRUST) PROPELLER PADA PESAWAT MODEL REMOTE CONTROL (UAV),” vol. 8, no. 1, 2022.
J. C. Kewas, M. Ali, J. Sains dan Teknologi, U. P. Negeri Manado T D Rompas, and J. Charles Kewas, “Analisis Gaya Angkat Akibat Perubahan Kecepatan Aliran Udara Dan Sudut Serang Pada Airfoil Naca 0015 Dalam Wind Tunnel Sub Sonic,” Jurnal Frontiers, vol. 3, no. 1, 2020, [Online]. Available: www.unima.ac.id/lppm/efrontiers
M. Anyoji, “High-performance airfoil with low reynolds-number dependence on aerodynamic characteristics,” Fluid Mechanics research International Journal, vol. 3, pp. 76–80, Jan. 2019, doi: 10.15406/fmrij.2019.03.00055.
G. Jatisukamto and M. Sari, “Analisis Airfoil Double-Slot Flap LS(01)-0417 MOD Dengan Airfoil Tanpa Flap Nasa SC(2) 0610,” Jurnal Energi Dan Manufaktur, vol. 11, no. 2, p. 49, Oct. 2018, doi: 10.24843/jem.2018.v11.i02.p03.
W. W. Salsabila S, “,” Jurnal Teknik ITS, vol. 9, no. 2, pp. B102–B107, 2020, Accessed: Dec. 19, 2022. [Online]. Available: https://ejurnal.its.ac.id/index.php/teknik/article/view/55639
P. V. M. P. Saroinsong H, “RANCANG BANGUN WAHANA PESAWAT TANPA AWAK (FIXED WING) BERBASIS ARDUPILOT - 2018,” Jurnal Teknik Elektro dan Komputer, vol. 7, pp. 73–84, 2018, Accessed: Dec. 19, 2022. [Online]. Available: https://ejournal.unsrat.ac.id/index.php/elekdankom/article/view/19195
U. Usin, Y. Fernanda, A. Karudin, and A. Kurniawan, “Comparison Lift and Drag of Airfoil NACA 1408 Standard and Modification Using Computational Fluid Dynamic,” MOTIVECTION : Journal of Mechanical, Electrical and Industrial Engineering, vol. 4, no. 3, pp. 223–236, Aug. 2022, doi: 10.46574/motivection.v4i3.146.
M. Yusuf Tamtomi, R. Sulistiyanti, and M. Komarudin, “ELECTRICIAN-Jurnal Rekayasa dan Teknologi Elektro Rancang Bangun Wahana Udara Tanpa Awak VTOL-UAV Sebagai Wahana Identifikasi Dini Kondisi Udara Berbasis Video Sender,” 2016.
S. Krishnamurthy, S. Jayashankar, S. V Rao, R. Krishna T S, and S. Nyamannavar, “CFD ANALYSIS OF AN RC AIRCRAFT WING,” 2014.
Dharmawan P, “Analisis Perbandingan Angle of Attack pada Airfoil Modifikasi dan NACA 0018 menggunakan Pendekatan Komputasional (CFD) - 2021,” Jurnal Kajian Ilmiah dan Teknologi Teknik Mesin (J-Proteksion), vol. 6, no. 1, pp. 20–25, Aug. 2021, Accessed: Dec. 20, 2022. [Online]. Available: http://jurnal.unmuhjember.ac.id/index.php/J-Proteksion
Diterbitkan
Cara Mengutip
Terbitan
Bagian
Lisensi
Hak Cipta (c) 2023 Minhajul Qowim

Artikel ini berlisensiCreative Commons Attribution-ShareAlike 4.0 International License.
An author who publishes in the J-ENSITEC (Journal of Engineering and Sustainable Technology) agrees to the following terms:
- Author retains the copyright and grants the journal the right of first publication of the work simultaneously licensed under the Creative Commons Attribution-ShareAlike 4.0 License that allows others to share the work with an acknowledgment of the work's authorship and initial publication in this journal
- The author is able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book) with the acknowledgment of its initial publication in this journal.
- The author is permitted and encouraged to post his/her work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of the published work