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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Xehetasun bibliografikoak

Egile nagusia:	FAISAL, KH. MD.
Formatua:	Tesis
Hizkuntza:	ingelesa
Argitaratua:	DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST) 2017
Gaiak:	LEADING EDGE ROTATING, CYLINDER, PERFORMANCE, SYMMETRIC AEROFOIL
Sarrera elektronikoa:	http://hdl.handle.net/123456789/257
Etiketak:	Etiketa erantsi Etiketarik gabe, Izan zaitez lehena erregistro honi etiketa jartzen!