Optimization of a3D Aircraft Morphing Wing with highly controllable Aerodynamic Performance
Anmol Krishna Mohan Chaudhary1, Deepan C2, Latshathipathi A3, Arun S.R4, Rakesh Kumar Shah5
1Anmol Krishna Mohan Chaudhary, Aeronautical Engineering, Excel Engineering College, komarapalayam, India.
2Deepan C, Aeronautical Engineering, Excel Engineering College, komarapalayam, India.
3Latshathipathi A, Aeronautical Engineering, Excel Engineering College, komarapalayam, India.
4Arun S R, Assistant Professor, Aeronautical Engineering, Excel Engineering College, Komarapalayam, India.
5Rakesh Kumar Shah, Aeronautical Engineering, Excel Engineering College, Komarapalayam, India.
Manuscript received on March 15, 2020. | Revised Manuscript received on March 24, 2020. | Manuscript published on March 30, 2020. | PP: 4295-4300 | Volume-8 Issue-6, March 2020. | Retrieval Number: F9141038620/2020©BEIESP | DOI: 10.35940/ijrte.F9141.038620
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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: The sole purpose of this project is to compare the aerodynamic performance of the modernistic wing with morphing techniques to the conventional one (i.e. wing with ailerons and flaps). The morphing wing is capable of enhancing the mission profiles through its significant geometrical changes in the surface areas (upper and lower area of wing). The primary aspiration is to calculate the CL and CD (coefficient of lift and drag) of real aircraft with conventional control surfaces and to compare its result with morphing wing. The morphing techniques also enables various prevention of aerodynamic losses (drag, vortices, noise, etc) caused due to geometrical discontinuities of conventional wing with aileron and flap in operating conditions (take-off, cruise, loiter, landing).Catia modelling of proposed wing is analysed by CFD method and to compare and contrast the aerodynamic performance with the conventional (hinged) wing.
Keywords: Adaptive Wing, Ansys, Catia, CFD, Fluent, Metamorphosis, Morphing, Wing Contour,
Scope of the Article: Discrete Optimization.