Նմանատիպ նյութեր: 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 /
Խորագիր: 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’ /
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- DEVELOPMENT OF AN EXPERIMENTAL SETUP FOR ANALYZING THE INFLUENCE OF MAGNUS EFFECT ON THE PERFORMANCE OF AIRFOIL /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
Խորագիր: This Thesis Paper of AE in B.Sc. Program.
- DEVELOPMENT OF MORTAR FIRING SIMULATOR FOR TRAINING AND PREDICTING THE ACCURACY OF IT'S PROJECTILE /
- COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /
- 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 /
- ANALYSIS OF FLOW DYNAMICS OF A NACA 2412 AIRFOIL WITH CAVITY THROUGH NUMERICAL SIMULATION AND WIND TUNNEL EXPERIMENT /
- STUDY OF THE FLOW FIELD ON THE UPPER SURFACE OF NACA 0015 & NACA 2418 AT DIFFERENT AANGLE OF ATTACK /
- STUDY AND COMPARATIVE ANALYSIS OF AERODYNAMIC CHARACTERISTICS AND IMPROVED PERFORMANCE OF NACA 0015 AIRFOIL WITH BLEED /