STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL

I wholeheartedly thank my supervisor Prof. Dr. M. A. Taher Ali, whose guidance, insight and instruction was the main essence of this study and without which the study would not be possible. I thank respected head of the Department of Mechanical Engineering, MIST, Brig Gen Md. Lutfor Rahman, PhD to...

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Hlavní autor:	FAISAL, KH. MD.
Médium:	Diplomová práce
Jazyk:	angličtina
Vydáno:	DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST) 2017
Témata:	LEADING EDGE ROTATING, CYLINDER, PERFORMANCE, SYMMETRIC AEROFOIL
On-line přístup:	http://hdl.handle.net/123456789/257
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!