Propeller locations study on delta-winged unmanned aerial vehicle (UAV) model
Delta wing design is being used in aircraft to obtain high manoeuvre properties. The flow above the delta wing is complicated and dominated by a very complex vortex structure. This research investigates the effects of the propeller locations on the aerodynamic characteristics above a generic 55° sha...
Saved in:
主要作者: | Kasim, Khushairi Amri |
---|---|
格式: | Thesis |
語言: | English |
出版: |
2017
|
主題: | |
在線閱讀: | http://eprints.utm.my/id/eprint/78655/1/KhushairiAmriKasimMFKM2017.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
-
The development of autopilot system for an unmanned aerial vehicle (UAV) helicopter model
由: Shamsudin, Syariful Syafiq
出版: (2007) -
Structural design improvement of unmanned aerial vehicle wing
由: Kanesan, Gunasegaran
出版: (2014) -
Superaugmentation and stability augmentation control system for unmanned aerial vehicle
由: Nogoud, Yasser Abdullah Mahjoub
出版: (2017) -
Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
由: Rashid, Rohayati Ab
出版: (2011) -
Autorotation performance of unmanned aerial vehicle helicopter using rectangular and quadratic blades
由: Mat Ali, Mohamed Sukri
出版: (2007)