Analysis of Engine and Propeller Selection for Unmanned Aircraft LSU-05 NG
Submitted : 2020-08-21, Published : 2020-10-31.
Abstract
This research focuses on analyzing the selection of engine and propeller for the propulsion system of LSU-05 NG by calculating the aircraft power needs. The aircraft power is evaluated in two loading conditions, namely heavy loading with regard to minimum take-off speed and light loading with regard to maximum cruise speed. Furthermore, from the five engine recommendations available, propeller rotation efficiency, thrust generated, and engine weight that meets the aircraft DRO (Design Requirment and Objective) are analyzed. The results of this research provide recommendations for using an engine with a minimum power of 16.5 hp with the main candidate is DLE 170 and a 32x10 size propeller as the LSU-05 NG propulsion system.
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A. Rizaldi, “LSU-05 NG Design Requirements and Objectives,” Bogor, Indonesia, 2019.
D. Anggraeni, A. R. Sumaryanto, E. Sumarna, and A. Rahmadi, “Engine and Propeller Selection for Propulsion System LAPAN Surveillance UAV – 05 (LSU-05) Using Analytic and Experimental Test,” in International Seminar of Aerospace Science and Technology II, 2014, pp. 41–50.
A. Balachandran, A. Shah, and D. J. Challa, “Propulsion Selection and Analysis for Unmanned Aerial Vehicles for SAE Aero Design Series,” Int. J. Eng. Sci., vol. 3, no. 8, pp. 29–35, 2014.
A. Dinç, “Sizing of a turboprop unmanned air vehicle and its propulsion system,” Isi Bilim. Ve Tek. Dergisi/ J. Therm. Sci. Technol., 2015.
I. T. Setyadewi and Y. A. Nugroho, “ANALISIS PEMILIHAN PROPELLER MESIN PESAWAT TANPA AWAK LSU 03,” Majalah Sains dan Teknologi Dirgantara, pp. 23–30, 2018.
“Flight Thrust, Power, and Energy Relations,” 2009. [Online]. Available: https://web.mit.edu/16.unified/www/SPRING/systems/Lab_Notes/airpower.pdf.
“Propeller Power Calculator.” [Online]. Available: http://www.mini-iac.no/wp-content/uploads/2012/11/prop-power-calculator-Neu-2230-1Y_15s_-Mejzlik.xls.
N. Atmasari et al., “ANALISIS PENENTUAN POWER LOADING PADA DESAIN AWAL PESAWAT TERBANG TANPA AWAK LSU-05 NG,” J. Teknol. Dirgant., vol. 17, pp. 109–122, 2019.
Dessert Aircraft Australia, DA 150 Owners Manual. Australia.
Dessert Aircraft Australia, DA 170 Owners Manual. Australia.
DLE Hobbico, DLE 170 Operator’s Manual. 2010.
MVVS, Operating Instructions MVVS 116 IRS No : 3010. Czech Republic.
Evolution gas Power Horizon Hobby, Evolution Engines 116GX2 User Guide. 2007.
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