Research on Combination of Swing Wing with Canard and Tail used in Fighter Aircraft
Praveen babu1, Swathi P Shetty2, Kavya G Achar3, Steve JohnsonLobo4, Lokesh K S5, Jagadeesh6
1Praveen babu, UG Scholar, Department of Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
2Swathi P Shetty, UG Scholar, Department of Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
3Kavya G Achar, UG Scholar, Department of Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
4Steve JohnsonLobo, UG Scholar, Department of Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
5Lokesh K S, Assistant Professor, Department of Mechanical & Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
6Jagadeesh, Assistant Professor, Department of Mechanical & Aeronautical Engineering, Srinivas Institute of Technology, Valachil, Mangaluru (Karnataka), India.
Manuscript received on 22 July 2019 | Revised Manuscript received on 03 August 2019 | Manuscript Published on 10 August 2019 | PP: 1057-1059 | Volume-8 Issue-2S3 July 2019 | Retrieval Number: B11970782S319/2019©BEIESP | DOI: 10.35940/ijrte.B1197.0782S319
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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 present work discloses the new design of a fighter aircraft. Better performance of a fighter in the combat as well in its ground activities is the main vision of our work. It is concentrating on the aircraft short distance take off and landing, stalling controlling, as well as different maneuverings of the aircraft. Many fighter aircraft are having its own working parameters and configurations. Every aircraft shown its own characteristics in flight like maneuverings, stalling etc.The major problem of them is prohibiting some of these characteristics in some angle of attack. So to control we have implemented some modifications. To achieve all these characteristics, we have selected the combination of swing wing with canard and tail configuration. By using this technology we can increase the flight ability to its maximum. So all the characteristics are in the control as we have designed.
Keywords: Aircraft Research Combination Design Characteristics.
Scope of the Article: Machine Design