Ähnliche Einträge: MULTICOPTER DRONE BASED AERIAL NETWORK FOR AUTONOMOUS OPERATION, DYNAMIC TARGET DETECTION & ANALYSIS /
- STABILITY AND PERFORMANCE ANALYSIS OF A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AND AIR DEFENCE SYSTEM TARGET DRONE /
- DESIGN AND FABRICATION OF A TARGET DRONE /
- PROPULSION SYSTEM OF A TARGET DRONE /
- DESIGN AND DEVELOPMENT OF TARGET DRONE: STABILITY AND CONTROL ANALYSIS /
- DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
- DESIGN AND FABRICATION OF A FIXED-WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING OF AIR DEFENSE SYSTEM /
Thema: 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 /
Thema: 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 /