Antzeko izenburuak: ANALYSIS OF FLOW DYNAMICS OF A NACA 2412 AIRFOIL WITH CAVITY THROUGH NUMERICAL SIMULATION AND WIND TUNNEL EXPERIMENT /
- Wind tunnels : models,aerodynamics and applications /
- COMPARATIVE STUDY OF BLOWING AND SUCTION SLOT GEOMETRY OPTIMIZATION ON NACA 0015 AND NACA 2412 AIRFOIL /
- CHARACTERISTIC ANALYSIS OF NACA 0018 AND NACA 2412 AIRFOIL WITH LEADING EDGE AND TRAILING EDGE ROTATING CYLINDER /
- SYNERGISTIC FLOW CONTROL: INGRATION OF DYNAMIC VORTEX GENERATORS AND VARYING DIMPLE GEOMETRIES FOR ENHANCED AERODYNAMIC CHARACTERISTICS FOR NACA 2412 AIRFOIL /
- PREDICTION OF ICE ACCRETION AND CFD ANALYSIS OF NACA 2412 AIRFOIL FOR EVALUATION OF AERODYNAMIC PERFORMANCE DEGRADATION
- PREDICTION OF ICE ACCRETION AND CFD ANALYSIS OF NACA 2412 AIRFOIL FOR EVALUATION OF AERODYNAMIC PERFORMANCE DEGRADATION /
Gaia: 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’’ /
Gaia: This Thesis Paper of AE in B.Sc. Program.
- EXPERIMENTAL STUDY OF MEAN FLOW CHARACTERISTICS OF SWIRLING JETS /
- STABILITY AND PERFORMANCE ANALYSIS OF A FIXED WING (UNMANNED AERIAL VEHICLE) TARGET DRONE FOR TESTING AND AIR DEFENCE SYSTEM TARGET DRONE /
- INVESTIGATION OF MECHANICAL PROPERTIES OF STIR CASTED AL6063/AL2O3 (ALUMINA) REINFORCED METAL MATRIX COMPOSITE /
- AERODYNAMIC ANALYSIS OF VARIABLE GEOMETRY RAKED WINGTIP /
- COGNITIVE STUDY ON RADAR PERFORMANCE ANALYSIS WITH THE EFFECT OF SENSITIVITY TIME CONTROL (STC) /
- FLOW CHARACTERISTICS AND HEAT TRANSFER CHARACTERISTICS OVER NACA 4415 AIRFOIL