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GPS-INS NEWLY PROPOSED INTEGRATED SYSTEM BASED ON KALMAN FILTER AND COMPLEMENTARY FILTER FOR AIRCRAFT POSITION DETERMINATION /
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DESIGN, CONSTRUCTION AND PERFORMANCE CHECKING OF A LOW COST & LIGHTER BLADE ANTENNA /
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DEVELOPMENT OF INTERACTIVE MULTIMEDIA PACKAGE ON AIRCRAFT INSTRUMENTS / Flg offr Mosammat Samia Khanam, Flg offer Shariaz Ebna Khalam, Md. Rashed Hossain
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DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
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DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
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SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
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DESIGN AND DEVELOPMENT OF INERTIAL MEASURMENT UNIT (IMU) IN ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FOR REAL TIME MANEUVER MONITORING OF LOW ALTITUDE AIRCRAFT BY USING KALMAN FILTER /
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MODIFICATION OF A TURBO-JET ENGINE (F-7 ENGINE) AS A TRAINING AID / Flg offr A.K.M.Tajul Islam, Flg offr Md. Sayed Jaber, Flg offr B.M.Anisuzzaman
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A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
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DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
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DESIGN AND FABRICATION OF AUTOMATIC FUEL TRANSFER SYSTEM OF AN AIRCRAFT /
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DESIGN OF MINIATURE TYPE PARALLEL COUPLED MICRO STRIP HAIR PIN FILTER IN VHF /
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STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
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DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
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DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
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A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
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ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
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A STUDY OF ELECTRONIC NAVIGATION SYSTEM AND OPTICAL INSTRUMENTS /
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DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
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DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
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DESIGN AND DEVELOPMENT OF MFD PAGES FOR FIGHTER AIRCRAFT USING FLIGHTGEAR FLIGHT SIMULATOR DATA OUTPUT /
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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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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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A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
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COMPARATIVE ASSESSMENT OF TURBULENCE OF IMPROVED PERFORMANCE OF NAC 0012 AIRFOIL WITH MSBLC /
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STUDY OF MULTI SPECIES NANO-PARTICLES TO ENHANCE THERMO-HYDRAULIC PERFORMANCE IN MICRO CHANNELS /
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STUDY OF THE EFFECT OF MOVING SURFACE BOUNDARY LAYER CONTROL ( MSBC) ON SINGLE & DOUBLE CYLINDER CONFIGURATION NACA 23018 AIRFOIL /
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AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
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A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
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PERFORMANCE ANALYSIS OF CENTRIFUGAL COMPRESSOR WITH AND WITHOUT SPLITTER BLADES /
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DESIGN AND FABRICATION OF AN AUTOPILOT MODEL TO INCORPORATE AUTOMATIC CONTROL OF THE MOMENT OF THE CONTROL SURFACES /
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MAINTENANCE & SERVICE MANUAL OF MIST X -1 /
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"DESIGN,FABRICATION AND DEVELOPMENT OF AN UNMANNED AERIAL VEHICLE CAPABLE OF DELIVERING MISSION PAYLOAD"
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DETECTION OF OBJECTS IN 2-D USING SONAR SENSOR /
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DESIGN & DEVELOPMENT OF RADAR COOLANT MONITORING , ALARMING AND CONTROLLING SYSTEM /
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EXPERIMENTAL STUDY OF FLOW CHARACTERISTICS AROUND NACA 4418 AND NACA 0012 AIRFOIL /
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A STUDY ON MULTIPLICATION DISPLAY AND SIMULATION OF MFD SYMBOLOGY /
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MODIFICATION OF A TURBO-JET ENGINE (F-7 ENGINE) AS A TRAINING AID / Flg offr A.K.M.Tajul Islam, Flg offr Md. Sayed Jaber, Flg offr B.M.Anisuzzaman
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STUDY OF FLOW OVER A FANWING IN A SUBSONIC WIND TUNNEL / Sajida Akter Jahan, Sadia Kamal Mery, Tarek Zobaer.
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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
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DESIGN AND FABRICATION OF AIRFRAME STRUCTURE & CONTROLS OF UAV / Md. Fazlay Robbey, Md. Mukit Hasan, Saiful Islam .
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ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
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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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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.
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DESIGN,ANALYSIS AND FABRICATION OF A FULLY ARTICULATED HELICOPTER MAIN ROTOR SYSTEM /
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DETERMINATION OF FLOW CHARACTERISTICS AND PERFORMANCE ANALYSIS OF THE NON-ROTATING & ROTATING CYLINDER /