Podobne zapisy: ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
- 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 /
- SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
Temat: 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 /
Temat: This Thesis Paper of AE in BSc Program.
- DESIGN AND IMPLEMENTATION OF A COORDINATE UAV SWARM FOR LONG RANGE OPERATIONS /
- DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
- DEVELOPMENT OF PROGAMMABLE HOT WIRE CNC MACHINE FOR AEROSTRUCTURE FABRICATION /
- MULTI-PHYSICS ANALYSIS OF FIBER-REINFORCED ANISOTROPIC COMPOSITES UNDER ELECTRO-THERMAL BOUNDARY CONDITIONS /
- ELECTROTHERMAL BEHAVIOR OF ANGLED FIBER-REINFORCED COMPOSITE LINES /
- THERMOMECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITE MATERIALS /
Autor: Shapneel, Maria Tabassum Shapneel
Autor: Supervised by Gp Capt Sidharth Sankar Patnaik
- EVALUATION OF STABILITY & PERFORMANCE ANALYSIS WITH MODIFICATION & OPTIMIZATION OF DESIGN OF A FIXED WING TARGET DRONE(UAV) FOR AIR DEFENSE SYSTEM /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- DESIGN AND FABRICATION OF AUTOMATIC FUEL TRANSFER SYSTEM OF AN AIRCRAFT /
- STUDY ON DIFFERENT KIND OF BOMB DEPLOYMENT SYSTEM AND ARMAMENT SEQUENCING OF AN AIRCRAFT /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /