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Analysis Of 6.3.1 Fabrication Of Wing Structure

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Analysis Of 6.3.1 Fabrication Of Wing Structure
6.3.1 Fabrication of Wing Structure: The wing the main components of RC as it is the part that is responsible for the lift and all the aerodynamic forces, angle of attack, Lift etc. are the depended on the Wing. For better lift, the wing structure should be better.
6.3.2 Structural Design
The large Wingspan means aero elasticity influences on aerodynamics and especially on dynamic stability and control. In order to minimize such interferences and movements in the solar array, the wing should have been designed to be rigid as possible. However, trade-offs with wing weight results in a slightly elastic wing.
6.3.2 Wind ribs:
Removing the indistinguishable wind ribs can be something of a task notwithstanding when a metal layout is utilized for cutting around. A simple, and exact, technique for using so as to create extensive number of wind ribs is two layouts, plywood, metal or plastic cover and sandwiching between them the required number and thickness of balsa sheet for the ribs. The balsa sheet for the rib spaces should be sliced just to harsh measurements as the full circuit is cut and sanded.
…show more content…
Full bi-axial plastic skin set wise from L.E to T.E with a strengthened forward D-box and beam, all produced in MDF molds, with few inner ribs from Balsa and foam (cut with knife).
6.3.3.1 Wing design Explanation

• We used Dihedral wing, which helps to increase the gliding time with use of less battery charge.
• Our wing is designed as high wing, because it is easy to fly for trainer aircraft.
• We used electric motor, which has the capability to carry 5 kg.
• Our UAV is used for proto type

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