相似書籍: ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- DEVELOPMENT OF A CFD MODEL FOR SIMULATING THE AERODYNAMIC PERFORMANCE OF A BLENDED WING BODY AIRCRAFT (WITH AND WITHOUT VORTEX GENERATOR) /
- EXPERIMENTAL STUDY ON THE EFFECT OF DIFFERENT WINGLET CONFIGURATIONS ON THE LIFT AND DRAG CHARACTERISTICS OF A BLENDED WING BODY AIRCRAFT /
- COMPARATIVE STUDY OF SHELL & TUBE HEAT EXCHANGER PERFORMANCE WITH & WITHOUT DELTA WINGLET VORTEX GENERATORS /
- SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
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- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
主題: Aeronautical Engineering
- 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 /
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- A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
主題: This Thesis Paper of AE in BSc Program.
- DESIGN DEVELOPMENT OF WEAPON CONTROL SYSTEM TO ACCOMMODATE GUIDED AMMUNITION AND ROCKET POD /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
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- DESIGN OF FUEL MANAGEMENT SYSTEM TO ADDRESS FAILURE IN AUTOMATIC FUEL TRANSFER SEQUENCE AND FABRICATE A REDUNDANCY SYSTEM /
- DEVELOPMENT OF AN OPEN SYSTEM ARCHITECTURE USING REAL-TIME DATA ACQUISITION AND TELEMETRY FOR EFFECTIVE FLIGHT DATA VISUALIZATION AND ANALYSIS /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
作者: Shapneel, Maria Tabassum Shapneel
作者: Supervised by Gp Capt Sidharth Sankar Patnaik
- 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 /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- EVALUATION OF STABILITY & PERFORMANCE ANALYSIS WITH MODIFICATION & OPTIMIZATION OF DESIGN OF A FIXED WING TARGET DRONE(UAV) FOR AIR DEFENSE SYSTEM /