-
STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER TRANSVERSE LOADING /
-
STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER SHEAR LOADING / Roohany Mahmud .
-
A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
-
DESIGN AND FABRICATION OF AN AUTOPILOT MODEL TO INCORPORATE AUTOMATIC CONTROL OF THE MOMENT OF THE CONTROL SURFACES /
-
SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF BOUNDARY VALUE PROBLEMS POLAR AND CYLINDRICAL COORDINATE SYSTEM / Farhan Hasan Nuri, Md. Shoriful Islam .
-
PROPERTIES AND MACHINABILITY OF SIC REINFORCED AL-BASED METAL MATRIX COMPOSITE UNDER CNT FLUID / Shafkat Z. Islam, Nawshin Sanjida Haque, Farzana Yeasmin,
-
ANALYSIS AND INSTALLATION OF AVIONICS SYSTEM IN A SMALL UNMANNED AIRCRAFT /
-
DESIGN AND DEVELOPMENT OF A COMBIND TORSION AND BENDING TEST SETUP FOR EVALUATING MECHANICAL PROPERTIES OF MATERIALS /
-
COMPARATIVE ASSESSMENT OF TURBULENCE OF IMPROVED PERFORMANCE OF NAC 0012 AIRFOIL WITH MSBLC /
-
DEVELOPMENT OF HYDRAULIC BENDING MACHINE /
-
A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
-
GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /
-
REVIEW OF OPTICAL FIVER DATA BUS AND FLY- BY LIGHT CONCEPT IN AVIATION /
-
DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
-
MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
-
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
-
DESIGN PROTOTYPE PROPOSAL OF OPTICAL FIBER BASED AVIONICS DATA BUS FOR A SMALL AIRCRAFT / S.M. Easin Ankur, Faisal Ahmed & Akter Mahmud Nafi .
-
STUDY OF FLOW CHARACTERISTIC OF A CIRCULAR JET / Umama Sharah Taskia, Maliha Yelmahi, Fatema Tarannum & Afifa Muna.
-
STUDY OF FLOW OVER A FANWING IN A SUBSONIC WIND TUNNEL / Sajida Akter Jahan, Sadia Kamal Mery, Tarek Zobaer.
-
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
-
DESIGN AND FABRICATION OF AIRFRAME STRUCTURE & CONTROLS OF UAV / Md. Fazlay Robbey, Md. Mukit Hasan, Saiful Islam .
-
MEASUREMENT OF DRUG GEOMETRIC MODELS APPLICATION OF FORCE MOMENTUM THEOREM /
-
ROLE OF COMPOSITES MATERIALS IN AEROSPACE APPLICATIONS – A REVIEW /
-
DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /