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Topic: This Thesis Paper of AE in BSc Program

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DESIGN DEVELOPMENT OF WEAPON CONTROL SYSTEM TO ACCOMMODATE GUIDED AMMUNITION AND ROCKET POD /
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ADAPTIVE DRONE PATH OPTIMIZATION USING D*LITE, NONLINEAR MODEL PREDICTIVE CONTROL AND B-SPLINE TRAJECTORY PLANNING /
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DESIGN AND IMPLEMENTATION OF A COORDINATE UAV SWARM FOR LONG RANGE OPERATIONS /
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DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
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SYNTHESIS AND CHARACTERIZATION OF JUTE-DERIVED CARBON MATERIALS FOR ADVANCED COMPOSITE AND WATER FILTRATION APPLICATIONS /
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DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
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DESIGN, FABRICATION,AND FLIGHT TESTING OF GHOST WING "GW-1" MAV /
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A FRAMEWORK FOR REAL-TIME HUMAN DETECTION AND AUTONOMOUS RESPONSE IN SWARM UAV-BASED SURVEILLANCE /
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EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF DIFFERENT CHEVRON NOZZLES /
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DEVELOPMENT OF PROGAMMABLE HOT WIRE CNC MACHINE FOR AEROSTRUCTURE FABRICATION /
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MULTI-PHYSICS ANALYSIS OF FIBER-REINFORCED ANISOTROPIC COMPOSITES UNDER ELECTRO-THERMAL BOUNDARY CONDITIONS /
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ELECTROTHERMAL BEHAVIOR OF ANGLED FIBER-REINFORCED COMPOSITE LINES /
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THERMOMECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITE MATERIALS /
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DESIGN AND DEVELOPMENT OF A COMBIND TORSION AND BENDING TEST SETUP FOR EVALUATING MECHANICAL PROPERTIES OF MATERIALS /
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SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
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DEFECT EVOLUTION AND SHOCK INDUCED PHASE TRANSFORMATION IN VNbTaTiZr REFACTORY HIGH ENTROPY ALLOY UNDER PROLONGED SHOCK COMPRESSION: A LARGE SCALE MOLECULAR DYNAMICS STUDY /
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PERFORMANCE ANALYSIS OF FIXED AND MORPHING WINGS USING NACA 4412 ASYMMETRIC AIRFOILS UNDER VARYING ANGLES OF ATTACK AND FLOW REGIMES /
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DIFFERENTIALLY PRIVATE MULTY-STAGE FLIGHT DELAY PREDICTION NETWORK (DP-MSFDPN): A PRIVACY-PRESERVING THREE-STAGE TEMPORAL CONVOLUTION FRAMEWORK /
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PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
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A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
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DESIGN OF FUEL MANAGEMENT SYSTEM TO ADDRESS FAILURE IN AUTOMATIC FUEL TRANSFER SEQUENCE AND FABRICATE A REDUNDANCY SYSTEM /
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DEVELOPMENT OF AN OPEN SYSTEM ARCHITECTURE USING REAL-TIME DATA ACQUISITION AND TELEMETRY FOR EFFECTIVE FLIGHT DATA VISUALIZATION AND ANALYSIS /
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ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
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THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /

Topic: Aeronautical Engineering

Author: Supervised by Mahbuba Ferdous

Author: Shahid, Nahian

Similar Items: DESIGN DEVELOPMENT OF WEAPON CONTROL SYSTEM TO ACCOMMODATE GUIDED AMMUNITION AND ROCKET POD /

Similar Items: ADAPTIVE DRONE PATH OPTIMIZATION USING D*LITE, NONLINEAR MODEL PREDICTIVE CONTROL AND B-SPLINE TRAJECTORY PLANNING /