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...

Description complète

Détails bibliographiques

Auteur principal:	FAISAL, KH. MD.
Format:	Thèse
Langue:	anglais
Publié:	DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST) 2017
Sujets:	LEADING EDGE ROTATING, CYLINDER, PERFORMANCE, SYMMETRIC AEROFOIL
Accès en ligne:	http://hdl.handle.net/123456789/257
Tags:	Ajouter un tag Pas de tags, Soyez le premier à ajouter un tag!