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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Autor principal:	FAISAL, KH. MD.
Formato:	Thesis
Idioma:	inglês
Publicado em:	DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST) 2017
Assuntos:	LEADING EDGE ROTATING, CYLINDER, PERFORMANCE, SYMMETRIC AEROFOIL
Acesso em linha:	http://hdl.handle.net/123456789/257
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