Những quyển sách tương tự: 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 /
- A SYSTEMS ENGINEERING APPROACH TO THE DETAIL DESIGN OF TAIL,TRIM AND PERFORMANCE ANALYSIS OF A SMALL REMOTELY PILOTED AIRCRAFT /
- DESIGN, ANALYSIS AND OPTIMIZATION OF A SMALL UNMANNED AIRCRAFT /
- DESIGN & DEVELOPMENT OF STRUCTURE OF A PROTOTYPE AIRCRAFT MIST EXPERIMENTAL-1 / Refaty Munni, Najifa Tasnim & Asif Bin Hossain.
Đề tài: Aeronautical Engineering
- COMPARATIVE STUDY OF SWIRL FLOW & JET FLOW /
- COMPARATIVE STUDY OF AIRCRAFT APPROACH AND LANDING PERFORMANCE USING ILS, MLS AND GLS /
- MANUFACTURE AND MISSION PERFORMANCE ANALYSIS OF SMALL UNMANNED AIRCRAFT’ /
- A COMPARISON OF EXPERIMENTAL WITH SIMULATION EFFECTIVE OF NACA 0012 AIRFOIL WITH BARE /
- EFFECT OF CROSS –SECTIONAL SHAPES ON FREE JET CHARACTERIZATION NUMERICAL AND EXPERIMENTAL INVESTIGATION FEASIBLE AND PERFORMANCE OF DIFFERENT EXHAUST GEOMETRY /
- PROPERTIES OF NATURAL POLYMER MATRIX COMPOSITE WITH VARIOUS FIBER ORIENTATIONS /
Đề tài: 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 FABRICATION ON VACUUM ASSISTED INFUSIUN MOLDING SETUP FOR FABRICATION OF FLAT AND CURVED COMPOSITE PANELS /
- DESIGN AND IMPLEMENTATION OF A COORDINATE UAV SWARM FOR LONG RANGE OPERATIONS /
- 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 /
Tác giả: Hasan, Toufiq
Tác giả: Supervised by Maj Md. Touhidur Rahman Evan
- A NUMERICAL ANALYSIS ON THE AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 2412 AEROFOILS WITH CURVED TRAILING-EDEG PLANFORM /
- 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 /