Numerical analysis of tubercles leading edge for unmanned aerial vehicle composite wing
The demand of Unmanned Aerial Vehicle (UAV) technology received growing interest from today’s engineers in designing and manufacturing the products within a short time and at reasonable price. The wide availability of modern and developing composite materials and the aid of computer s...
Saved in:
主要作者: | Basri, Ernnie Illyani |
---|---|
格式: | Thesis |
語言: | English |
出版: |
2020
|
主題: | |
在線閱讀: | http://psasir.upm.edu.my/id/eprint/85600/1/FK%202020%2056%20-%20ir.pdf |
標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
相似書籍
-
Computational analysis of double rotating cylinders for conceptual design of an estol, fixed wing UAV
由: Alias, Mohd Shahidi
出版: (2017) -
Avian-inspired feature-based relative positioning strategy for formation control of multiple unmanned aerial vehicles
由: Mohamed Yaghoobi, Yousef Jassim Ismail Abdulla
出版: (2019) -
Unmanned aerial vehicle power estimation with non-polarity charging system
由: Hadi, Al Obaidi Mohammed Rmaez
出版: (2019) -
Constructing and calibrating unmanned aerial vehicle hexacopter with lightweight visible, near-infrared and thermal sensor for remote sensing (Not for loan)
由: Mansor, Ya'akob
出版: (2018) -
Mathematical Modelling of an Unmanned Aerial Vehicle
由: Chong, Chiew Choy
出版: (2005)