Míreanna comhchosúla: 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.
Topaic: 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’ /
- EFFECT OF MOMENTUM INJECTION ON THE PERFORMANCE OF AIRFOIL (MOVING SURFACE BOUNDARY LAYER CONTROL /
- DEVELOPMENT OF AN EXPERIMENTAL SETUP FOR ANALYZING THE INFLUENCE OF MAGNUS EFFECT ON THE PERFORMANCE OF AIRFOIL /
- PERFORMANCE OPTIMIZATION OF A VARIABLE GEOMETRICAL WING:ANALYSIS AND DESIGN OF MORPHING WING FOR UNMANNED AERIAL VEHICLE /
Topaic: This Thesis Paper of AE in BSc Program.
- 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 /
- DEVELOPMENT OF PROGAMMABLE HOT WIRE CNC MACHINE FOR AEROSTRUCTURE FABRICATION /
- MULTI-PHYSICS ANALYSIS OF FIBER-REINFORCED ANISOTROPIC COMPOSITES UNDER ELECTRO-THERMAL BOUNDARY CONDITIONS /
- ELECTROTHERMAL BEHAVIOR OF ANGLED FIBER-REINFORCED COMPOSITE LINES /
- THERMOMECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITE MATERIALS /
Údar: Hasan, Toufiq
Údar: 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 /