Նմանատիպ նյութեր: ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
Խորագիր: Aeronautical Engineering
- 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 /
- DESIGN & MODELING OF RADAR CONTROL SYSTEM FOR DETECTING AIRCRAFT & MISSILE /
- A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
Խորագիր: This Thesis Paper of AE in BSc Program.
- DESIGN DEVELOPMENT OF WEAPON CONTROL SYSTEM TO ACCOMMODATE GUIDED AMMUNITION AND ROCKET POD /
- PASSIVE CONTROL OF WING ROCK IN A DELTA WING AIRCRAFT /
- A NUMERICAL STUDY ON THE OPTIMUM STRUCTURAL DESIGN OF AN AIRCRAFT TIRE TREAD /
- DESIGN OF FUEL MANAGEMENT SYSTEM TO ADDRESS FAILURE IN AUTOMATIC FUEL TRANSFER SEQUENCE AND FABRICATE A REDUNDANCY SYSTEM /
- DEVELOPMENT OF AN OPEN SYSTEM ARCHITECTURE USING REAL-TIME DATA ACQUISITION AND TELEMETRY FOR EFFECTIVE FLIGHT DATA VISUALIZATION AND ANALYSIS /
- ANALYZING AERO-STRUCTURAL BEHAVIOUR OF CONVENTIONAL AIRCRAFT WINGS THROUGH COMPUTATIONAL APPROACH AND EXPERIMENTAL VALIDATION /
Հեղինակ: Perves, Sifat
Հեղինակ: 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 /