Development of morphing UAV

Morphing wings are the subject of intensive research interest today due to their potential to improve aircraft versatility for multiple mission requirements. This report focuses on the development of a morphing UAV model with variable wing camber which is able to transform between airfoil NACA...

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Main Author: Tan, Chun Sing.
Other Authors: Jorg Uwe Schluter
Format: Final Year Project
Language:English
Published: 2012
Subjects:
Online Access:http://hdl.handle.net/10356/50355
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-503552023-03-04T19:35:58Z Development of morphing UAV Tan, Chun Sing. Jorg Uwe Schluter Liu Yong School of Mechanical and Aerospace Engineering DRNTU::Engineering::Mechanical engineering Morphing wings are the subject of intensive research interest today due to their potential to improve aircraft versatility for multiple mission requirements. This report focuses on the development of a morphing UAV model with variable wing camber which is able to transform between airfoil NACA23015 with E423. The morphing mechanism is designed and fabricated, and to be actuated by electrical servo motors. These changing in airfoil profile allow the UAV to maximize lift during take-off and landing, while minimizing drag during cruising. The morphing mechanism is carefully evaluated and tested, all the critical supporting structures are being analyzed using the finite element method, to ensure that the UAV is able to sustain under the designed loading parameters. Despite the variable camber, the UAV also incorporate the feasibility of variable swept wing for future research purposes. The wing box is built to include the variable swept wing mechanism, and the 3 points flexural test is conducted on the wing box structure, to ensure that the wing box is able to withstand the moment generated by the wings. Next, the fuselage of the UAV is built, which includes the selection and evaluation of motor as well as installation of landing gears. Finally, test fly is conducted to study the improvement of flying characteristic that brought by the morphing wings. Bachelor of Engineering (Mechanical Engineering) 2012-06-01T04:10:22Z 2012-06-01T04:10:22Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50355 en Nanyang Technological University 99 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering
spellingShingle DRNTU::Engineering::Mechanical engineering
Tan, Chun Sing.
Development of morphing UAV
description Morphing wings are the subject of intensive research interest today due to their potential to improve aircraft versatility for multiple mission requirements. This report focuses on the development of a morphing UAV model with variable wing camber which is able to transform between airfoil NACA23015 with E423. The morphing mechanism is designed and fabricated, and to be actuated by electrical servo motors. These changing in airfoil profile allow the UAV to maximize lift during take-off and landing, while minimizing drag during cruising. The morphing mechanism is carefully evaluated and tested, all the critical supporting structures are being analyzed using the finite element method, to ensure that the UAV is able to sustain under the designed loading parameters. Despite the variable camber, the UAV also incorporate the feasibility of variable swept wing for future research purposes. The wing box is built to include the variable swept wing mechanism, and the 3 points flexural test is conducted on the wing box structure, to ensure that the wing box is able to withstand the moment generated by the wings. Next, the fuselage of the UAV is built, which includes the selection and evaluation of motor as well as installation of landing gears. Finally, test fly is conducted to study the improvement of flying characteristic that brought by the morphing wings.
author2 Jorg Uwe Schluter
author_facet Jorg Uwe Schluter
Tan, Chun Sing.
format Final Year Project
author Tan, Chun Sing.
author_sort Tan, Chun Sing.
title Development of morphing UAV
title_short Development of morphing UAV
title_full Development of morphing UAV
title_fullStr Development of morphing UAV
title_full_unstemmed Development of morphing UAV
title_sort development of morphing uav
publishDate 2012
url http://hdl.handle.net/10356/50355
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