Gelijkaardige items: PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- STUDENT ANALYSIS OF AIRCRAFT WINGS WITH VARIOUS CONDITIONS /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- DESIGN & FABRICATION OF WING CONTROLS,UNDERCARRIAGE AND SKIN OF HOME BUILT EXPERIMENTAL AIRCRAFT’’ MIST X-01’’ /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
Onderwerp: Aeronautical Engineering
- ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
- DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
- MEASUREMENT OF DRUG GEOMETRIC MODELS APPLICATION OF FORCE MOMENTUM THEOREM /
- A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
- GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /
- REVIEW OF OPTICAL FIVER DATA BUS AND FLY- BY LIGHT CONCEPT IN AVIATION /
Onderwerp: This Thesis Paper of AE in BSc Program.
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- MULTICOPTER DRONE BASED AERIAL NETWORK FOR AUTONOMOUS OPERATION, DYNAMIC TARGET DETECTION & ANALYSIS /
- DESIGN AND PARAMETRIC ANALYSIS OF H-PLANE HORN & MICROSTRIP PATCH ANTENNA AT X-BAND FOR INTERFERENCE SUPPERESION /
- ADAPTIVE DRONE PATH OPTIMIZATION USING D*LITE, NONLINEAR MODEL PREDICTIVE CONTROL AND B-SPLINE TRAJECTORY PLANNING /
Auteur: Afroz, Ashika
Auteur: 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 /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /