Channels - DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / :: Library Catalog

Eitemau Tebyg: DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM /

Pwnc: Thesis Paper of AE in B.Sc Prog.

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COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
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COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
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MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
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A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
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EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
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PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
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A COMPREHENSIVE STUDY OF FLOW THROUGH CIRCULAR PIPE /
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MODELING AND SIMULATION OF LONGITUDINAL AUTOPILOT FOR GENERAL AVIATION AIRCRAFT /
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DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
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MACHINABILITY OF POLYMER MATRIX COMPOSITES (PMC)-A REVIEW OF CURRENT STATUS AND FUTURE PROSPECTS /
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ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
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STRUCTURAL ANALYSIS OF AIR CRAFT WINGS WITH VARIOUS CONDITIONS /
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DESIGN AND CONSTRUCTION OF LOW ATTITUDE HEADING REFERENCE SYSTEM (AHRS) BASED ON MICRO ELECTRO MECHANICAL SYSTEM WITH INTEGRATED IMU IN REAL TIME /
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DEVELOPMENT OF MICRO CONTROLLER BASED AVIONICS PACKAGE WITH REAL TIME FLIGHT VISUALIZATION EMERGENCY AUTO LANDING AND FLIGHT DATA RECORDER /
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DESIGN OF MINIATURE TYPE PARALLEL COUPLED MICRO STRIP HAIR PIN FILTER IN VHF /
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STUDY AND DESIGNING OF MICRO CONTROLLER BASED TEMPERATURE SENSING SYSTEM ALONG WITH GLOBAL SYSTEM FOR MOBILE INTERFACE AND ALARM MECHANISM TO BE USED IN EFFERENT TEMPERATURE SENSITIVE STOREHOUSES /
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DESIGN AND FABRICATION OF A GAS GENERATOR USING AN AUTO MOBILE TURBOCHARGER /
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SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF BOUNDARY VALUE PROBLEMS POLAR AND CYLINDRICAL COORDINATE SYSTEM / Farhan Hasan Nuri, Md. Shoriful Islam .
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STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER SHEAR LOADING / Roohany Mahmud .
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DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
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INVESTIGATION OF DRAG EFFECT OF AROFOIL SHAPED FUSELAGE UAV MODEL AND VISUALIZATION OF AIR FLOW / Captain Md. Ruhul Amin Noor, Flying Officer Syeda Lira Rayhan & Flying Officer Umme Laila Amin
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DESIGN PROTOTYPE PROPOSAL OF OPTICAL FIBER BASED AVIONICS DATA BUS FOR A SMALL AIRCRAFT / S.M. Easin Ankur, Faisal Ahmed & Akter Mahmud Nafi .
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STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
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DEVELOPMENT OF AIRCRAFT SYSTEM DEMONSTRATOR: FOUGA CM170 MAGISTER AIRCRAFT / Capt Arif Md. Amirul Abrar, Capt A Ashigur Rahman Sany, Hannanur Rashid Saddam.

Pwnc: Aeronautical Engineering.

Awdur: Evan, Md. Tauhid Rahman

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DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian

Awdur: Md. Tauhid Rahman Evan

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DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian