Modeling of a Radio Controlled Plane with Analysis of Lift Generation Using Ansys Fluent
K. Rajesh Kumar1, D. Sreenivasulu Reddy2
1K. Rajesh Kumar, Assistant Professor, Department of Mechanical Engineering, MTIET, Palamaner, Chittor (Andhra Pradesh), India.
2Dr. D.Sreenivasulu Reddy, M.Tech, Ph.D. HOD & Associate Professor, Department of Mechanical Engineering, MTIET, Palamaner, Chittor  (Andhra Pradesh), India.
Manuscript received on 10 January 2019 | Revised Manuscript received on 20 January 2019 | Manuscript Published on 30 January 2019 | PP: 98-103 | Volume-8 Issue-2S2, January 2019 | Retrieval Number: B10220182S219/19©BEIESP
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Abstract: Aircraft are important, because they carry people and goods quickly to great distant places, over all types of terrains. From the only last century we were all certain that the aircraft flies The basic forces that are associated with the flight are the Lift, Drag, Thrust and Weight. We are clear with the Thrust is created by the fly motors because of the response powers produced by fumes gases and is given by Newton’s third law and Due to the consistency of air when aircraft travels through air we have Drag over the aircraft and any item having mass will have Weight due to earths pull But we are not clear how the Lift is generated which is most important of the four forces acting on aircraft. There are two different ways of clarifying the lift generation on wing. One is the numerical description which is depicted by utilizing course ideas and the other is the physical depiction of lift. Despite the fact that we have numerous physical portrayals of lift does not fulfill in all conditions Thus we demonstrated an airplane with cambered aerofoil alongside the investigation is made in Ansys Fluent that how the lift is created which is the verification for the Actual physical depiction of lift.
Keywords: Lift, Drag, Coanda Effect and RC (Radio Controlled).
Scope of the Article: Quality Control