Computational analysis of double rotating cylinders for conceptual design of an estol, fixed wing UAV
Many efforts in Unmanned Aerial Vehicle (UAV) aerodynamic design technology led to a broad of additional applications. Magnus effect is the effect of moving airstream to the spinning ball or cylinder. Previous studies revealed the feasibility of Magnus effect on rotating cylinder producing lift whic...
محفوظ في:
المؤلف الرئيسي: | Alias, Mohd Shahidi |
---|---|
التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2017
|
الموضوعات: | |
الوصول للمادة أونلاين: | http://psasir.upm.edu.my/id/eprint/76076/1/FK%202018%20156%20-%20IR.pdf |
الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
مواد مشابهة
-
Numerical analysis of tubercles leading edge for unmanned aerial vehicle composite wing
بواسطة: Basri, Ernnie Illyani
منشور في: (2020) -
Analysis of one way valve mechanism for wings of a flapping drone /
بواسطة: Deng, Xinchen
منشور في: (2020) -
UAV-based extraction of topograhic and as-built information by object-based image analysis technique
بواسطة: Sibaruddin, Hairie Ilkham
منشور في: (2018) -
A new hybrid control algorithm design and simulated for Longitude and latitude movements stabilization of nonlinear fixed-wing UAV
بواسطة: Faizan, Ahmed Warsi -
Constructing and calibrating unmanned aerial vehicle hexacopter with lightweight visible, near-infrared and thermal sensor for remote sensing (Not for loan)
بواسطة: Mansor, Ya'akob
منشور في: (2018)