Experimental analysis on the inner vortices interaction above diamond wing model in low speed aerodynamics
Every country needs a high-speed Unmanned Air Vehicle (UAV) to monitor territory especially their ocean. One of the best UAV that can perform this mission is Unmanned Combat Air Vehicle (UCAV). The main advantage of the UCAV is a kind of delta-shaped drone that can fly at high speed and greater alti...
Saved in:
主要作者: | Said, Mazuriah |
---|---|
格式: | Thesis |
語言: | English |
出版: |
2021
|
主題: | |
在線閱讀: | http://eprints.utm.my/id/eprint/99519/1/MazuriahSaidPSKM2021.pdf.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
-
Further Evaluation Of Aerodynamic Characteristics Of The Aero 3 Trainer Aircraft Wing
由: Thirunavakarasu, Prakash
出版: (2000) -
Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
由: Rashid, Rohayati Ab
出版: (2011) -
Diffuser augmented wind turbine for low-speed wind
由: Elsherbeiny, Mohamed Mohamed Takeyeldein
出版: (2022) -
Design and development of diamond grinding wheel for ultra precision applications
由: Etminan, Payam
出版: (2010) -
Drag reduction of wing-in-ground craft by using micro
vortex generator
由: Irahasira, binti said
出版: (2021)