STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /

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Korporativní autor:	Supervised by Wg Cdr Dr. G.M. Jahangir Alam (Sr. Instructor, Dept. of ME, MIST.)
Další autoři:	Asaduzzaman, K.M, Arman, Arif
Médium:	Kniha
Jazyk:	angličtina
Vydáno:	Dhaka : ME DEPT. MIST, c2014.
Témata:	Mechanical Engineering This Thesis Paper of ME in B.Sc. Program.
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!

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040		\|a BD-DhMIS \|c BD-DhMIS
100		\|4 Rahman, Irfanur
245		\|a STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE / \|c Irfanur Rahman, K.M. Asaduzzaman, Arif Arman
260		\|a Dhaka : \|b ME DEPT. MIST, \|c c2014.
300		\|a 84p. : \|b ill. ; \|c 29 cm
504		\|a Includes bibliographical references.
541		\|e TP-1047
650		\|a Mechanical Engineering
650		\|a This Thesis Paper of ME in B.Sc. Program.
700		\|a Asaduzzaman, K.M.
700		\|a Arman, Arif
710		\|a Supervised by Wg Cdr Dr. G.M. Jahangir Alam \|e Sr. Instructor, Dept. of ME, MIST.
942		\|2 ddc \|c TP
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