Podobné jednotky: 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 /
Téma: Aeronautical Engineering.
- DESIGN,ANALYSIS AND FABRICATION OF A FULLY ARTICULATED HELICOPTER MAIN ROTOR SYSTEM /
- DETERMINATION OF FLOW CHARACTERISTICS AND PERFORMANCE ANALYSIS OF THE NON-ROTATING & ROTATING CYLINDER /
- DESIGN AND OPTIMIZATION OF LOW SPEED WIND TURBINE WITH MOMENTUM INJECTION /
- STUDY ON MECHANICAL BEHAVIOR OF SISAL AND BANANA FIBER REINFORCED POLYMER MATRIX COMPOSITES /
- A STUDY OF FLOW THROUGH CIRCULAR PIPE /
- EVALUATION OF THE INFLUENCE OF CARBON NANO PARTICLES ON THE MECHANICAL BEHAVIOR OF PARTICLES ON THE MECHANICAL BEHAVIOR OF BANANA FIBER REINFORCED POLYMER COMPOSITE /
Téma: 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 /