STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
This project and dissertation is a significant outcome of supreme guidance and concentrated team effort. We respectfully acknowledge the cordial help of individuals who played distinct role for the successful accomplishment of the project. We offer our deepest gratitude to our supervisor Wg Cdr Dr G...
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| Những tác giả chính: | , , |
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| Định dạng: | Luận văn |
| Ngôn ngữ: | Tiếng Anh |
| Được phát hành: |
Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST)
2016
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| Những chủ đề: | |
| Truy cập trực tuyến: | http://hdl.handle.net/123456789/245 |
| Các nhãn: |
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| Tóm tắt: | This project and dissertation is a significant outcome of supreme guidance and concentrated team effort. We respectfully acknowledge the cordial help of individuals who played distinct role for the successful accomplishment of the project. We offer our deepest gratitude to our supervisor Wg Cdr Dr G.M Jahangir Alam, psc, senior instructor; Department of Mechanical Engineering (MIST).His tremendous contribution, excellent guidance and depth of knowledge in the relevant field lead our project to a perfect completion.
We are also indebted to the faculty members of Department of Mechanical Engineering, (MIST) for the required additional support. We thank MIST for providing us with the required funding for implementing the project. We would like to express our humble gratitude to all the mechanics, technicians, and lab assistants of MIST workshop for rendering us technical support.
Last but not the least; we acknowledge the support and patience of our parents who allowed us necessary freedom during the completion of the project. Above all we praise and thank the almighty Allah for the success of the project. |
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