Míreanna comhchosúla: ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
Topaic: Aeronautical Engineering
- ACTIVE CONTROL OF FLOW PAST OVER NACA 0021 THROUGH LEADING EDGE MOMENTUM INJECTION USING ROTATING CYLINDER: A COMPARATIVE INVESTINGATION BETWEEN NUMERICAL & EXPERIMENTAL ANALYSIS/
- DESIGN AND DEVELOPMENT OF A BLADE ANTENNA FOR AIRCRAFT NAVIGATION AND COMMUNICATION /
- MEASUREMENT OF DRUG GEOMETRIC MODELS APPLICATION OF FORCE MOMENTUM THEOREM /
- A STUDY OF IMPROVEMENTS ENGINES PERFORMANCE APPLYING INTERCHANGEABILITY ASSOCIATED WITH RAIN AND A NEW APPROACH OF GNESS BASED LANDING SYSTEM /
- GROUND SUPPORT EQUIPMENT OF ‘’ MIST X – 1’’ /
- REVIEW OF OPTICAL FIVER DATA BUS AND FLY- BY LIGHT CONCEPT IN AVIATION /
Topaic: This Thesis Paper of AE in BSc Program.
- THERMOMECHANICAL BEHAVIOR OF FIBER-REINFORCED COMPOSITE MATERIALS /
- DESIGN AND DEVELOPMENT OF A COMBIND TORSION AND BENDING TEST SETUP FOR EVALUATING MECHANICAL PROPERTIES OF MATERIALS /
- SUPERSONIC FLOW CONTROL IN COMPRESSION CORNER BY MICRO-VORTEX GENERATOR AND MICRO-JET /
- DEFECT EVOLUTION AND SHOCK INDUCED PHASE TRANSFORMATION IN VNbTaTiZr REFACTORY HIGH ENTROPY ALLOY UNDER PROLONGED SHOCK COMPRESSION: A LARGE SCALE MOLECULAR DYNAMICS STUDY /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- THERMO-MECHANICAL ANALYSIS OF AIRCRAFT STRUCTURES REINFORCED WITH STIFFENERS /
Údar: Perves, Sifat
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 /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
- A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /