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COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
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DESIGN AND DEVELOPMENT OF FUEL SYSTEM & LANDING GEAR FOR TARGET DRONE /
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A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
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Aircraft Design:A conceptual approach
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Aircraft Design:A conceptual approach
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DEVELOPMENT OF A PHASED OUT AIRCRAFT AS EDUCATIONAL AID /
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DESIGN OPTIMIZATION OF WORM GEAR /
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ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
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ANALYSIS OF OPERATIONAL LIMIT OF AN AIRCRAFT: AN AEROELASTIC APPROACH /
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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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STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
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DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
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MODELING AND SIMULATION OF LONGITUDINAL AUTOPILOT FOR GENERAL AVIATION AIRCRAFT /
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MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
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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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DEVELOPMENT OF MICRO CONTROLLER BASED AVIONICS PACKAGE WITH REAL TIME FLIGHT VISUALIZATION EMERGENCY AUTO LANDING AND FLIGHT DATA RECORDER /
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DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
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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 AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,
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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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DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
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LARGE DEFECTION ANALYSIS OF AN AIRCRAFT WING WITH ELLIPTICAL LIFT DISTRIBUTION AT DIFFERENT FLIGHT CONDITION /
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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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DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
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PROPERTIES AND MACHINABILITY OF SIC REINFORCED AL-BASED METAL MATRIX COMPOSITE UNDER CNT FLUID / Shafkat Z. Islam, Nawshin Sanjida Haque, Farzana Yeasmin,
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DESIGN OF CAMBERED AEROFOIL FOR UNMANNED AERIAL VEHICLE BASED ON SUBSONIC WIND TUNNEL TEXT / KH. Md. Faisal Md. Faisal Kabir, Nahian Al Hossain Basunia,
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DESIGN AND IMPLEMENTATION OF A LAW COST ATTITUDE HEADING REFERENCE SYSTEM FOR LAW SPEED AIRCRAFT / Md. Shajid-Ul-Mahmud, Tariqul Islam, Md. Saiful Islam,
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INVESTIGATION FOR PROSPECT OF RECLAIMED ASPHALT PAVEMENT (RAP) TO BE USED AS STABILIZED BASED IN THE CONTEXT OF BANGLADESH / Maj Md Tasfiqur Rahman.
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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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AIRCRAFT RETRACTABLE LANDING GEAR AUTOMATION A CONCEPTUAL APPROACH / Rana Ashique ,