“Multi Swept Wing”– Elite Execution Over Wing’s History
Ramesh Kumar1, Sabarikumar M2, Vignesh S3, Boopathi D4, Ranga Raj R5
1Mr. Rameshkumar R, Final year, Department of Aeronautical Engineering, Sri Ramakrishna Engineering College, Coimbatore (Tamil Nadu), India.
2Mr. Sabarikumar M, Final year, Department of Aeronautical Engineering, Sri Ramakrishna Engineering College, Coimbatore (Tamil Nadu), India.
3Mr. Vignesh S, Final year, Department of Aeronautical Engineering, Sri Ramakrishna Engineering College, Coimbatore (Tamil Nadu), India.
4Mr. Boopathi D, Final year, Department of Aeronautical Engineering, Sri Ramakrishna Engineering College, Coimbatore (Tamil Nadu), India.
5Mr. Ranga Raj R, Assistant Professor, Department of Aeronautical Engineering, Sri Ramakrishna Engineering College, Coimbatore (Tamil Nadu), India.
Manuscript received on 6 April 2014 | Revised Manuscript received on 17 April 2014 | Manuscript Published on 30 April 2014 | PP: 85-90 | Volume-3 Issue-11, April 2014 | Retrieval Number: K16120431114/14©BEIESP
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: Profundity of wing structure that needs change has no closure. A wing is a type of fin with surface that produce aerodynamic force for aircraft through the atmosphere, In that way, a high performance aircrafts capable of subsonic, transonic and supersonic speed employ a forward swept wing platform. Due to aero elasticity effect, the aerodynamic force on wing tip tends to bend it in forward swept wing. But in the wing design that we propose, has smaller elasticity effect. The air flows towards the wing root and hence the dangerous tip stall becomes safer in our wing. Also due to sweep at the tip of the wing, it increases the aileron performance and further it increases the yaw directional stability. Since the wings are generally larger at the root and due to multi swept, this improves the lift performance. As a result, maneuverability is improved especially at both lower and higher angle of attacks. Thus the stability of a forward swept wing aircraft is disclosed that corrects a dynamic instability phenomenon which occurs when the whole vehicle (rigid body) motion couples with the wing structural motion. Our technology will be elite in wing’s ability today.
Keywords: Aerodynamics, Improved Lift and Drag, Maneuverability, Multi Swept, Stability.
Scope of the Article: Multi-Agent Systems