Eitemau Tebyg: INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
- 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
- SURFACE MODIFICATION OF NACA 4418 AIRFOIL WITH DIFFERENT SHAPED DIMPLES AND AERODYNAMIC PERFORMANCE ANALYSIS /
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
- SHAPE OPTIMIZATION OF GURNEY FLAP ON AIRFOIL /
- EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
- STABILITY AND PERFORMANCE ANALYSIS OF A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AND AIR DEFENCE SYSTEM TARGET DRONE /
Pwnc: Aeronautical Engineering.
- COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
- COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
- MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
- A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
- EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
Pwnc: This Thesis Paper of AE in B.Sc. Program.
- DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
- ANALYSIS OF DESIGN FLAWS IN AN UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE AND FABRICATION, CFD ANALYSIS AND TUNNEL TESTING OF A 3D MODEL POST AMENDMENT /
- DESIGN AND FABRICATION OF A TARGET DRONE /
- SHAPE OPTIMIZATION OF GURNEY FLAP ON AIRFOIL /
- FABRICATION OF AL-6063 METAL MATRIX HYBRID COMPOSITE REINFORCED WITH SIC NANOPARTICALS BY STRI CASTING /
- DESIGN & DEVELOPMENT OF A SOFTWARE TOOL FOR ANALYSIS OF THE CHARACTERISTICS OF INSTRUMENTED RECTILINEAR OPEN LOOP CONTROL SYSTEM /