000 02521ntm a2200253 a 4500
001 vtls000082912
003 KUKTEM
005 20251117113232.0
008 141104t2013 my da f m 000 0 eng d
020 _aTHE0007381(Local)
039 9 _a201905151134
_bfawwaz
_c201411131322
_dtraining1
_c201411041138
_dtraining1
_c201411041045
_dtraining1
_y201411041013
_ztraining1
040 _aUMP
090 _aTL589.4 .M64 2013 r Bc.
100 0 _aMoganaraj Murugiah
245 1 0 _aDetail experimental testing of unmanned aerial vehicles engine performance/
_cMoganaraj Murugiah
260 _aKuantan, Pahang :
_bUMP,
_c2013
300 _axiv, 76 p. : ill. (some col.) ;
_c30 cm. +
_e1 CD-ROM
502 _aProject Paper (Bachelors of Mechanical Engineering) -- Universiti Malaysia Pahang – 2013
504 _aBibliography : p. 48-49
520 3 _aThis project is about detail experimental testing of Unmanned Aerial Vehicles (UAV) engine performance. However, there is no proper selection of test bed available for the performance evaluation, testing and analysis of the UAV propulsion system. This project has two major objectives which are to design and fabricate a test bed for the UAV propulsion system and to conduct detail performance experimentations of the UAV propulsion system run at various speed. In this study, test bed model is designed to test the nitro engine Unmanned Aerial Vehicle (UAV) which is model of Thunder Tiger Pro36 Engine Series of aircraft performance. In addition, six performance parameters are recorded for testing of the engine performance, which are Thrust, shaft brake power, available power, propulsive efficiency, specific fuel consumption and thrust coefficient. Furthermore, the method used in this project is to identify the unknown variables in parameters by using some sensors. The results show that the fabricated test bed can be used to study the engine performance. Specifically, performance parameters are directly proportional to the engine speed. These results show that the performance parameters are increasing along with the speed. In conclusion, the fabricated test bed can be used for the testing of engine performance analysis. Outcomes of this experiment can be successful by using the test bed because it helps to reduce the cost and time for UAV propulsion performances testing.
650 0 _aDrone aircraft
_xAutomatic control
650 0 _aGuidance systems (Flight)
999 _aVIRTUA40
_c5170
_d5176
999 _aVTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5040*5200*6500*6501*9992