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...
Saved in:
Main Author: | Koh, Hui Wei |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Final Year Project |
Language: | English |
Published: |
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10356/60434 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Redesign, analysis, fabrication and testing of light weight wing for solar UAV : part 2
by: Oh, Ying Qun
Published: (2014) -
Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : part 1
by: Yap, Kelvin Bing Hui
Published: (2014) -
Redesign, analysis, fabrication and testing of light weight fuselage, boom and empennage for solar UAV : Part 3
by: Tan, Thomas Peng Ngee
Published: (2015) -
Solar UAV : design, fabrication and testing of a test wing section and integration with solar cells
by: Pang, Yida.
Published: (2012) -
Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing
by: Chua, Zac Zheng Xun.
Published: (2013)