Ähnliche Einträge: STUDY AND DEVELOPMENT OF MOVING TARGET LOCATION AND RANGE ACQUIRING SYSTEM ALONG WITH GUI TO INCORPORATE IN A PROTOTYPE LOW-COST ACTIVE PHASED ARRAY RADAR /
- STUDY AND DEVELOPMENT OF MOVING TARGET LOCATION AND RANGE ACQUIRING SYSTEM ALONG WITH GUI TO INCORPORATE IN A PROTOTYPE LOW-COST ACTIVE PHASED ARRAY RADAR.
- ANALYSIS OF RADAR SIGNAL USING MICROSTRIP ANTENNA FOR SELECTING OPTIMUM THRESHOLD IN ORDER TO DESIGN & FABRICATE A PROTOTYPE LOW-COST ACTIVE PHASES ARRAY /
- ACQUISITION & ANALYSIS OF TIME DOMAIN RAW DATA TO DEVELOP A GRAPHICAL USER INTERFACE IN ORDER TO DESIGN & FABRICATE A PROTOTYPE LOW-COST ACTIVE PHASED ARRAY RADAR /
- ANALYSIS OF RADAR CROSS SECTION (RCS) OF DIFFERENT SHAPE OF TARGETS USING MICROSTRIP ANTENNA IN ORDER TO DESIGN & FABRICATE A PROTOTYPE OF LOW COST PHASED ARRAY RADAR /
- ANALYSIS OF RADAR CROSS SECTION (RCS) OF DIFFERENT SHAPE OF TARGETS USING MICROSTRIP ANTENNA IN ORDER TO DESIGN & FABRICATE A LOW COST ACTIVE PHASED ARRAY RADAR /
- ACQUISITION & ANALYSIS OF TIME DOMAIN RAW DATA TO DEVELOP A GRAPHICAL USER INTERFACE FOR DESIGNING & FABRICATION OF A PROTOTYPE OF LOW - COST PHASED ARRAY RADAR /
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 /
- A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
- DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
- STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
Thema: This Thesis Paper of AE in B.Sc. Program.
- 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 /
- A STUDY OF FLOW THROUGH CIRCULAR PIPE /
- NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /