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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| Materyal Türü: | Tez |
| Dil: | İngilizce |
| Baskı/Yayın Bilgisi: |
DEPARTMENT OF MECHANICAL ENGINEERING MILITARY INSTITUTE OF SCIENCE AND TECHNOLOGY (MIST)
2017
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| Online Erişim: | http://hdl.handle.net/123456789/257 |
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| Özet: | 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 give me the permission to use Machine Tools Lab as well as Workshop of Mechanical Engineering Department.
Again I heartily thank the Head of the Department of Aeronautical Engineering, Group Captain Md. Abdus Salam, Bangladesh Air Force for providing me with opportunities and facilities of the office and the laboratory to conduct this thesis.
Wing Commander Dr. Vikram V. Deshpande, Indian Air Force, Instructor Class-A of Department of Aeronautical Engineering, MIST extended his guidance throughout the whole process for CFD simulation. I want to express my gratitude for his valuable time and relentless inspiration.
I want to express my gratitude towards Mr. Dibakar Tarafdar whose valuable craftsmanship made excellent contributions to the test section modification and manufacturing of newly developed setup. These works are valuable assets of this study. I thank Mr. Aminul Islam who helped me for assembly and disassembly of different parts as required during carrying out the experiments. |
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