Low-cost of fix-wing prototype using Zimmerman design
This paper discussed the design and development of a fix-wing UAV that uses a Zimmerman parameter. To increase structural strength, a material made of expanded polypropylene and expanded polystyrene was used. Using a bagging vacuum technique for 24 hours, the structural strength procedure thoroughly...
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| Format: | Article |
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Semarak Ilmu Publishing
2023
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| _version_ | 1796984165889998848 |
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| author | Mansor, Yaakob Omar Baki, Sharudin Mohd Noor, Ikhwan Syafiq Mohd Tarmizi, Emma Ziezie Abdul Aziz, Nor Azah |
| author_facet | Mansor, Yaakob Omar Baki, Sharudin Mohd Noor, Ikhwan Syafiq Mohd Tarmizi, Emma Ziezie Abdul Aziz, Nor Azah |
| author_sort | Mansor, Yaakob |
| collection | UPM |
| description | This paper discussed the design and development of a fix-wing UAV that uses a Zimmerman parameter. To increase structural strength, a material made of expanded polypropylene and expanded polystyrene was used. Using a bagging vacuum technique for 24 hours, the structural strength procedure thoroughly combines the resin and fiber. The Zimmerman graph, generated at speeds between 50,000 and 200,000 using Reynolds Numbers (RE), was analyzed using three key variables: the coefficient of lift, drag, and the angle of attack (Alpha) of the airfoil. At 10o, the airfoil started to stall based on indicated coefficient used. The test flight is also comprised of pitch and roll flight with adequate force and little overshoot between the autopilot's requirement and the small aircraft's actual performance. |
| first_indexed | 2024-03-06T11:16:37Z |
| format | Article |
| id | upm.eprints-102108 |
| institution | Universiti Putra Malaysia |
| last_indexed | 2024-03-06T11:16:37Z |
| publishDate | 2023 |
| publisher | Semarak Ilmu Publishing |
| record_format | dspace |
| spelling | upm.eprints-1021082023-08-18T23:51:32Z http://psasir.upm.edu.my/id/eprint/102108/ Low-cost of fix-wing prototype using Zimmerman design Mansor, Yaakob Omar Baki, Sharudin Mohd Noor, Ikhwan Syafiq Mohd Tarmizi, Emma Ziezie Abdul Aziz, Nor Azah This paper discussed the design and development of a fix-wing UAV that uses a Zimmerman parameter. To increase structural strength, a material made of expanded polypropylene and expanded polystyrene was used. Using a bagging vacuum technique for 24 hours, the structural strength procedure thoroughly combines the resin and fiber. The Zimmerman graph, generated at speeds between 50,000 and 200,000 using Reynolds Numbers (RE), was analyzed using three key variables: the coefficient of lift, drag, and the angle of attack (Alpha) of the airfoil. At 10o, the airfoil started to stall based on indicated coefficient used. The test flight is also comprised of pitch and roll flight with adequate force and little overshoot between the autopilot's requirement and the small aircraft's actual performance. Semarak Ilmu Publishing 2023-01-01 Article PeerReviewed Mansor, Yaakob and Omar Baki, Sharudin and Mohd Noor, Ikhwan Syafiq and Mohd Tarmizi, Emma Ziezie and Abdul Aziz, Nor Azah (2023) Low-cost of fix-wing prototype using Zimmerman design. Journal of Advanced Research in Applied Sciences and Engineering Technology, 29 (1). pp. 237-244. ISSN 2462-1943 https://semarakilmu.com.my/journals/index.php/applied_sciences_eng_tech/article/view/1260 10.37934/araset.29.1.237244 |
| spellingShingle | Mansor, Yaakob Omar Baki, Sharudin Mohd Noor, Ikhwan Syafiq Mohd Tarmizi, Emma Ziezie Abdul Aziz, Nor Azah Low-cost of fix-wing prototype using Zimmerman design |
| title | Low-cost of fix-wing prototype using Zimmerman design |
| title_full | Low-cost of fix-wing prototype using Zimmerman design |
| title_fullStr | Low-cost of fix-wing prototype using Zimmerman design |
| title_full_unstemmed | Low-cost of fix-wing prototype using Zimmerman design |
| title_short | Low-cost of fix-wing prototype using Zimmerman design |
| title_sort | low cost of fix wing prototype using zimmerman design |
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