Redesign, analysis, fabrication and testing of light weight wing with solar panels as wing skin for solar UAV : part 1
This report is on the design of a Solar Unmanned Aerial Vehicle (UAV) of mission requirement of Medium Altitude Long Endurance. The report focuses on the airframe configuration and design in the structural aspect of the UAV especially with respect to the wing. The first part of the report covers ana...
محفوظ في:
المؤلف الرئيسي: | Koh, Hui Wei |
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مؤلفون آخرون: | School of Mechanical and Aerospace Engineering |
التنسيق: | Final Year Project |
اللغة: | English |
منشور في: |
2014
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الموضوعات: | |
الوصول للمادة أونلاين: | http://hdl.handle.net/10356/60434 |
الوسوم: |
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مواد مشابهة
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Redesign, analysis, fabrication and testing of light weight wing for solar UAV : part 2
بواسطة: Oh, Ying Qun
منشور في: (2014) -
Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : part 1
بواسطة: Yap, Kelvin Bing Hui
منشور في: (2014) -
Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : Part 3
بواسطة: Tan, Thomas Peng Ngee
منشور في: (2015) -
Solar UAV : design, fabrication and testing of a test wing section and integration with solar cells
بواسطة: Pang, Yida.
منشور في: (2012) -
Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing
بواسطة: Chua, Zac Zheng Xun.
منشور في: (2013)