Please use this identifier to cite or link to this item:
http://hdl.handle.net/10603/287103
Title: | Finite Element Analysis on Performance Of Cropped Delta Wing Aircraft with Fence |
Researcher: | Arun M P |
Guide(s): | Satheesh M |
Keywords: | Engineering and Technology,Engineering,Engineering Mechanical |
University: | Noorul Islam Centre for Higher Education |
Completed Date: | 25/01/2019 |
Abstract: | ABSTRACT newline newline newline newline newlineManufacturing and maintaining different aircraft fleet leads to various purposes, which consumes more money as well as manpower. Solution to this, nations that are leading in the field of aeronautics are performing much research and development works on new aircraft designs that could do the operations those were done by varied aircrafts. The foremost benefit of this delta wing is, along the huge rearward sweep angle, the wing s leading edge would not contact the boundary of shock wave. Further, the boundary is produced at the fuselage nose due to the speed of aircraft approaches and also goes beyond the transonic to supersonic speed. Further, rearward sweep angle greatly worse the airspeed:wings under normal condition to leading edge, so permits the aircraft to fly at great transonic, subsonic, or supersonic speed, whereas the overwing speed is kept to minimal range than that of the sound speed. Certain benefits are also there with the delta wing, and they are increase in transsonic drag is steady and supersonic flight s peak drag is compacted. Further, it reduces the sensitivity of drag to mach number. With all these considerations, this research work tries to make some advanced design strategy of delta wing by modelling and analysing as well. Further, the goal of this study is to utilize different means of delta wing modelling that facilitates the work in different fields. newlineIn the first contribution, the modelling of the delta wing under the aerodynamic view by software Catia V5 and analysis it. This research work simply focuses on wing plan design and that is functionally efficient. Furthermore, this work refers to certain conventional deltas like Mirages, Mig-21, XF-Convair, the Mirage III, and Eurofighter Typhoon. At last, it is identified that the Eurofighter Typhoon is the victorious design at maximum speeds however it remains unstable in low speeds. As the second contribution, the cropped delta wing under Catia V5 software has analysed in two cases: with fence and without fence as well. |
Pagination: | 173 |
URI: | http://hdl.handle.net/10603/287103 |
Appears in Departments: | Department of Mechanical Engineering |
Files in This Item:
File | Description | Size | Format | |
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acknowledgement.pdf | Attached File | 287.39 kB | Adobe PDF | View/Open |
certificate.pdf | 137.49 kB | Adobe PDF | View/Open | |
chapter 1.pdf | 617.42 kB | Adobe PDF | View/Open | |
chapter 2.pdf | 582.07 kB | Adobe PDF | View/Open | |
chapter 3.pdf | 457.12 kB | Adobe PDF | View/Open | |
chapter 4.pdf | 1.64 MB | Adobe PDF | View/Open | |
chapter 5.pdf | 995.18 kB | Adobe PDF | View/Open | |
chapter 6.pdf | 343.28 kB | Adobe PDF | View/Open | |
chapter 7.pdf | 621.16 kB | Adobe PDF | View/Open | |
chapter 8.pdf | 98.92 kB | Adobe PDF | View/Open | |
references.pdf | 4.24 MB | Adobe PDF | View/Open | |
title page.pdf | 88.83 kB | Adobe PDF | View/Open |
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