CD Skripsi
Perancangan Wahana Terbang Tanpa Awak Dengan Kemampuan Vertical Take-Off Landing (Vtol) Tipe Quadplane Dual System
ABSTRACT
Vertical Take-Off and Landing Fixed Wing (VTOL fixed wing) is a vehicle designed to combine the capabilities of rotary wing vehicle and fixed wing vehicle in one single vehicle platform. The quadplane dual-system is the most popular fixed wing VTOL concept. The development of fixed wing VTOL vehicles that has been carried out has several obstacles including being unstable during the take-off and landing process due to the use of three motors, a small MTOW to limit the load carried, and low flight time. For this reason, in this study, the design of a quadplane dual system type fixed-wing VTOL flying vehicle with a simpler, stable configuration and relatively large MTOW. The process of designing ride models using Solidworks 2019 software. Then the calculation of the aerodynamic characteristics of the ride was carried out using the ANSYS Fluent software. The results of aerodynamic calculations show that the ride cruise mode has an elevator coefficient of 1.1017 and a drag coefficient of 0.1044. Structural calculations are performed using ANSYS Static Structural software. The results of structural calculations show that the ride cruise mode has a deflection value of 15.901 mm at the end of the wing (chord tip). The maximum stress that occurs is 10,654 MPa on the wing spar. The lowest safety factor value occurred on the wing with a value of 3.403. In the take-off mode, a maximum deflection value of 5.0291 mm was obtained on the VTOL motor mount. The maximum stress is 10,834 MPa on the wing spar. The lowest safety factor value is 2.2464. With an energy consumption to perform the mission of 205,502 Wh, the battery used is a 4s battery with a capacity of 15000 mAh with an output of 222 Wh.
Keywords: VTOL, Quadplane, Fixed Wing, Ansys, Solidwork
Tidak tersedia versi lain