STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
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| Язык: | английский |
| Опубликовано: |
Dhaka :
ME DEPT. MIST,
c2014.
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Нет меток, Требуется 1-ая метка записи!
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