समान संसाधन: SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
- ANALYSIS OF AERODYNAMIC PERFORMANCE OF BLENDED WING BODY WITH VORTEX GENERATORS AND WINGLETS /
- COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
- EXPERIMENTAL STUDY OF MEAN FLOW CHARACTERISTICS OF SWIRLING JETS /
- NUMERICAL INVESTIGATION OF LIFT AUGMENTATION WITH CO-FLOW JET AIRFOIL /
- EXPERIMENTAL STUDY OF THE FLOW FIELD OF AN ANNULAR JET COALESCING AT THE EXIT /
- DESIGN AND FABRICATION OF A MICRO UAV WITH DEVELOPMENT OF ITS STRUCTURE, PROPULSION AND CONTROL SYSTEM / Md. Tauhid Rahman Evan, Mir Md. Al Kahman Tamal, Md. Jamal Mian
विषय: Aeronautical Engineering.
- DIFFERENTIALLY PRIVATE MULTY-STAGE FLIGHT DELAY PREDICTION NETWORK (DP-MSFDPN): A PRIVACY-PRESERVING THREE-STAGE TEMPORAL CONVOLUTION FRAMEWORK /
- STRESSES IN AN ANGLE PLY LAMINATED CANTILEVER UNDER TRANSVERSE LOADING /
- DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
- SYNTHESIS AND CHARACTERIZATION OF JUTE-DERIVED CARBON MATERIALS FOR ADVANCED COMPOSITE AND WATER FILTRATION APPLICATIONS /
- DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
- DESIGN, FABRICATION,AND FLIGHT TESTING OF GHOST WING "GW-1" MAV /
विषय: This Thesis Paper of AE in BSc Program.
- DIFFERENTIALLY PRIVATE MULTY-STAGE FLIGHT DELAY PREDICTION NETWORK (DP-MSFDPN): A PRIVACY-PRESERVING THREE-STAGE TEMPORAL CONVOLUTION FRAMEWORK /
- DESIGN AND FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
- SYNTHESIS AND CHARACTERIZATION OF JUTE-DERIVED CARBON MATERIALS FOR ADVANCED COMPOSITE AND WATER FILTRATION APPLICATIONS /
- DESIGN AND COMPUTATIONAL ANALYSIS OF SUBSONIC LOITER MUNITION'S WING USING DIFFERENT AIRFOIL SECTION /
- DESIGN, FABRICATION,AND FLIGHT TESTING OF GHOST WING "GW-1" MAV /
- A FRAMEWORK FOR REAL-TIME HUMAN DETECTION AND AUTONOMOUS RESPONSE IN SWARM UAV-BASED SURVEILLANCE /