ANALISIS PENENTUAN POWER LOADING PADA DESAIN AWAL PESAWAT TERBANG TANPA AWAK LSU-05 NG
DOI:
https://doi.org/10.30536/j.jtd.2019.v17.a3162Keywords:
power loading, estimasi, matching chart, optimalAbstract
Penelitian ini berfokus pada analisa penentuan power loading pada awal desain pesawat LSU-05 NG. Dengan menentukan power loading maka kebutuhan daya engine untuk pesawat LSU-05 NG dapat diestimasi. Artinya pemilihan engine dapat dilakukan sehingga menghasilkan gaya dorong agar pesawat dapat melakukan misi pemantauan dan foto udara dengan baik. Metode yang digunakan untuk analisa penentuan power loading adalah teknik Matching Chart atau Matching Plot dengan memilih titik optimal dari lima konstrain yaitu jarak take-off, climb rate, stall speed, cruise speed, dan landing. Hasil penelitian menunjukkan bahwa dengan massa 85 kg dan luas sayap 3,22 m2 pesawat LSU-05 NG membutuhkan daya 9.7 hp. Penjelasan lebih detail akan dijabarkan pada bagian selanjutnya.References
Banal, L. F., & Ubando, A. T. (2016). Fuzzy programming approach to UAV preliminary sizing. In 8th
International Conference on Humanoid, Nanotechnology, Information Technology, Communication and
Control, Environment and Management, HNICEM 2015. https://doi.org/10.1109/HNICEM.2015.7393239
Chipade, V. S., Abhishek, Kothari, M., & Chaudhari, R. R. (2018). Systematic design methodology for
development and flight testing of a variable pitch quadrotor biplane VTOL UAV for payload delivery.
Mechatronics. https://doi.org/10.1016/j.mechatronics.2018.08.008
Cinar, G., Emeneth, M., & Mavris, D. N. (2016). A Methodology for Sizing and Analysis of Electric
Propulsion Subsystems for Unmanned Aerial Vehicles. In 54th AIAA Aerospace Sciences Meeting. https://doi.org/10.2514/6.2016-0216
Coleman, Evan, Dan Deaver, Brandon Nowak, and Michael Rubino. 2014. Sizing of a Single-Engine
Propeller-Driven Aircraft. New York.
Dinç, A. (2015). Sizing of a turboprop unmanned air vehicle and its propulsion system. Isi Bilimi Ve
Teknigi Dergisi/ Journal of Thermal Science and Technology.
Essari, A. (2015). Estimation Of Component Design Weights In Conceptual Design Phase For Tactical
UAVs. University of Belgrade.
Federal Aviation Administration. (2011). AC 23-8C - Flight Test Guide for Certification of Part 23
Airports.
Ferreira, J. L. (2018). Conceptual Design of a Manned Reconnaissance Airplane for Martian Atmospheric
Flight. San Jose State University.
Glīzde, N. (2018). Wing and Engine Sizing by Using the Matching Plot Technique. Transport and
Aerospace Engineering. https://doi.org/10.1515/tae-2017-0018
Gunaseelan, V. K. (2011). Rapid Design and Virtual Testing of UAV the DEE Framework. Delft University
of Technology.
Harasani, W. (2010). Design, Build and Test an Unmanned Air Vehicleتصميم وبناء
وبرمجة طائرة بدون طيار. Journal of King Abdulaziz University-
Engineering Sciences. https://doi.org/10.4197/eng.21-2.6
Kamal, A. M., Serrano, A. R. (2018). Design methodology for hybrid (VTOL + Fixed Wing) unmanned
aerial vehicles. Canada.
Kidane, B. S. (2016). Design of Light GA Aircraft for Agricultural Purpose. University of Turkish.
Monterroso, A. (2018). Preliminary sizing, flight test, and Performance Analysis of Small Tri-Rotor VTOL
and Fixed Wing UAV. San Diego State University.
Raymer, D. P. (1992). Aircraft Design: A Conceptual Approach (Second Edi). Washington D.C: American
Institute of Aeronautics and Astronautics, Inc.
Rizaldi, A. (2019). LSU-05 NG Design Recquirements and Objectives. Bogor,Indonesia.
Roskam, J. (2005). Airplane Design. Vol. 1. Lawrence, Kansas.
Sadraey, M. (2013). A Systems Engineering Approach to Unmanned Aerial Vehicle Design. https://doi.org/10.2514/6.2010-9302
Seeckt, K., Scholz, D., & Tor, B. (2010). Application of the Aircraft Preliminary Sizing Tool Presto To
Kerosene and Liquid Hydrogen Fueled Regional Freighter Aircraft. Dlrk, 137–148.
Turanoguz, E. (2014). Design Of a Medium Range Tactical UAV And Improvement Of its Performance by
Using Winglets. Middle East Technical University.
Tyan, M., Nguyen, N. Van, & Lee, J. (2016). A Hybrid VTOL-Fixed Wing Electric UAV Sizing Methodology
Development, (October).
Tyan, Maxim, Nhu Van Nguyen, Sangho Kim, and Jae Woo Lee. 2017. “Comprehensive Preliminary
Sizing/Resizing Method for a Fixed Wing – VTOL Electric UAV.†Aerospace Science and Technology.
Yadav, S. (2014). Sizing of Aircraft According to Takeoff Distance Requirement. Retrieved June 16, 2019,
from https://surjeetyadav.wordpress.com/category/aircraft-design-2/
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Copyright (c) 2019 Novita Atmasari, Eries Bagita Jayanti, Nur Mufidatul Ula, M. Luthfi Ramadiansyah, Redha Akbar Ramadhan , Prasetyo Ardi Probo Suseno, Ardian Rizaldi, Kurnia Hidayat, Angga Septiyana
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