Míreanna comhchosúla: DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- COMPARATIVE STUDY OF SHELL & TUBE HEAT EXCHANGER PERFORMANCE WITH & WITHOUT DELTA WINGLET VORTEX GENERATORS /
- CFD SIMULATION OF FLOW AROUND 3D SUBMARINE SHAPED BODY
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
Topaic: 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 /
Topaic: 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 /