Development of Motorised Monoplane Wings for Educational Kit
This research in regards to development of motorised monoplane wings for educational kit is significant to study the performance of aircraft in many aspects. Such things required an investigate tool to study and investigate the behaviour and condition of fluid flow around the airfoil and any related issues at certain condition. In this study, the apparatus use is DC Combo Meter. By utilizing this apparatus, the power source use is Li-Po battery 2200mAh analyses for cases number of continuous discharge current. Compared to the experimental, this method has higher cost but very effective in terms of getting data to analyse. The target of this experiment is to consider how airplane fly up in the air, the connection between lift and drag coefficients at various speed flows. Results obtain from the experiment is important with a specific end goal to encourage other researchers and engineers that review in a similar field which may benefits them. The result shows the changes the value of lift and drag coefficient because of the speed flow and angle of attack. The result also present of the pressure along the surface of the airfoil that also gives effect of the lift and drag force. Besides, the results of the A2212 Brushless Motor demonstrate the thrust or velocity of the airplane to take-off which are greatly influenced by angle of attack of the wing structure. Therefore, there are many elements for the airplane to fly up in the air which should be decided so that it can be fully optimized.