Main Article Content
Abstract
Election electric motor as main motor engine and propeller as mechanical device of propulsion system Flying Wing PX aircraft has been done. The types of investigated electrics motor are EMAX BL 2382/05, NTM Pprop Drive Series 42-58 and Turnigy 3648. The propellers that have been tested are 12x8, 13x8, 14x7 and 15x7 dimension propeller. Parameters that have been investigated are power, velocity of motor, velocity of propeller and thrust. Effect of parameters on aircraft performance has been analyzed. Power as result from motor currents multiplied 11,1 volt baterai voltage. Velocities of motors as result from value of KV that technical term for explain how many motor rotation each second in 1 volt applied voltage. Propeller velocities were measured by Tachometer device. Air flow velocities were measured by Digital Anemometer Air Flow Meter. Furthermore, it’s used for thrust calculation. The result showed that the highest power and motor velocities obtained by EMAX BL 2382/05 is 888 watts and 8935 rpm. With the 888 watts as highest power, the aircraft is able to do sport performance. The propeller velocities which is appropriate with motor velocities maximum limit is 13x8 and 14x7 dimensions, but the highest thrust obtained by 14x7 dimensions. Thus, EMAX BL 2382/05 electric motor and 14x7 dimension propeller can used at Flying Wing PX aircraft in order to aircraft performance is maximal.
Keywords
Article Details

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
References
- (1) Dendhi, G., 2013. BLDC Motor,
- http://gerry24dendhi.blogspot.com/2013/12/bldc-motor.html diakses tanggal 20 Agustus 2015
- (2) Atmoko, B., _____, Merakit Sendiri
- Pesawat Terbang Model R/C, http://bandung-aeromodeling.com/tutorials/Engine_dan_Motor_Pesawat_Model.pdf, diakses pada 28 Januari 2016
- (3) _____, 2003, Sistem Propulsi
- Electrical,http://www.oocities.org/tinbd g/sistem-propulsi-elictrical.htm, diakses pada 21 Agustus 2015
- (4) Surya, Y., 2010, Desain Pesawat
- Masa Depan,
- http://www.ilmuterbang.com/artikel-mainmenu-29/teori-penerbangan-mainmenu-68/384-desain-pesawat-masa-depan diakses tanggal 27 Januari 2016
- (5) Hastono, A.N., 2015, Rancang Bangun
- Pesawat Model UAV Flying Wing PX dan Pemilihan Motor Listrik Berdasarkan Tiga Tipe Motor Brushless, Skripsi, Prodi Teknik Penerbangan Universitas Suryadarma, Jakarta
- (6) Michael, 2005, Brusless Convenrsion,
- http://miketigabelas.webs.com/brushless.html diakses tanggal 20 Mei 2015
- (7) Prakoso, A., 2015, Performa Propeller
- Pada Pesawat Flying Wing PX Dengan Motor Brushless Melalui Variasi Efisiensi Propeller Berdasarkan Konfigurasi Panjang Propeller, Skripsi, Prodi Teknik Penerbangan Universitas Suryadarma, Jakarta
- (8) Arismunandar, W., 2002,
- PengantarTurbin Gas dan Motor Propulsi, ITB Bandung.
References
(1) Dendhi, G., 2013. BLDC Motor,
http://gerry24dendhi.blogspot.com/2013/12/bldc-motor.html diakses tanggal 20 Agustus 2015
(2) Atmoko, B., _____, Merakit Sendiri
Pesawat Terbang Model R/C, http://bandung-aeromodeling.com/tutorials/Engine_dan_Motor_Pesawat_Model.pdf, diakses pada 28 Januari 2016
(3) _____, 2003, Sistem Propulsi
Electrical,http://www.oocities.org/tinbd g/sistem-propulsi-elictrical.htm, diakses pada 21 Agustus 2015
(4) Surya, Y., 2010, Desain Pesawat
Masa Depan,
http://www.ilmuterbang.com/artikel-mainmenu-29/teori-penerbangan-mainmenu-68/384-desain-pesawat-masa-depan diakses tanggal 27 Januari 2016
(5) Hastono, A.N., 2015, Rancang Bangun
Pesawat Model UAV Flying Wing PX dan Pemilihan Motor Listrik Berdasarkan Tiga Tipe Motor Brushless, Skripsi, Prodi Teknik Penerbangan Universitas Suryadarma, Jakarta
(6) Michael, 2005, Brusless Convenrsion,
http://miketigabelas.webs.com/brushless.html diakses tanggal 20 Mei 2015
(7) Prakoso, A., 2015, Performa Propeller
Pada Pesawat Flying Wing PX Dengan Motor Brushless Melalui Variasi Efisiensi Propeller Berdasarkan Konfigurasi Panjang Propeller, Skripsi, Prodi Teknik Penerbangan Universitas Suryadarma, Jakarta
(8) Arismunandar, W., 2002,
PengantarTurbin Gas dan Motor Propulsi, ITB Bandung.
