פריטים דומים: A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
- "A REVIEW ON EXPERIMENTAL STUDY OF AIRCRAFT TIRE TREAD PROPERTIES" /
- THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
- DESIGN OF A BANDPASS FILTER FOR AIRCRAFT COMMUNICATION /
- DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
- A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
- DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
נושא: Aeronautical Engineering
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /
- STUDY MEASUREMENT AND REDUCTION OF RADAR CROSS SECTION (RCS) /
- DESIGN & DEVELOPMENT OF THRUST PROVIDER FOR A HOME BUILT AIRCRAFT (MIST-EXPERIMENTAL-1) /
- STUDY OF GNSS AND ANALYSIS OF ITS IMPROVEMENT FOR POSITIONING ACCURACY /
- DESIGN , CONSTRUCTION AND PERFORMANCE CHECKING OF BLADE ANTENNA /
- DESIGN FEASIBILITY STUDY AND TECHNOLOGY DEMONSTRATION FOR DARAF ,MARKER ,BEACON, AUTO TAXING AND DIGITAL FLIGHT DATA RECORDER /
נושא: This Thesis Paper of AE in BSc Program.
- ADAPTIVE DRONE PATH OPTIMIZATION USING D*LITE, NONLINEAR MODEL PREDICTIVE CONTROL AND B-SPLINE TRAJECTORY PLANNING /
- DESIGN AND IMPLEMENTATION OF A COORDINATE UAV SWARM FOR LONG RANGE OPERATIONS /
- 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 /
מחבר: Hasan, Toufiq
מחבר: Supervised by Maj Md. Touhidur Rahman Evan
- A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /