Ejemplares similares: DETECTION OF OBJECTS IN 2-D USING SONAR SENSOR /
- AERODYNAMICS PERFORMANCE ANALYSIS OF 2D AIRFOIL/ NACA 4418 INCORPORATING WITH ROTATING CYLINDER /
- DATA FUSION OF IMU SENSORS AND ERROR REDUCTION USING KALMAN FILTER /
- DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
- STUDY AND DESIGNING OF MICRO CONTROLLER BASED TEMPERATURE SENSING SYSTEM ALONG WITH GLOBAL SYSTEM FOR MOBILE INTERFACE AND ALARM MECHANISM TO BE USED IN EFFERENT TEMPERATURE SENSITIVE STOREHOUSES /
- DESIGN AND FABRICATION OF A GAS GENERATOR USING AN AUTO MOBILE TURBOCHARGER /
- COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
Tópico: Aeronautical Engineering.
- Aeronautical radio communication systems and networks /
- 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’’ /