Eitemau Tebyg: STUDY OF FLOW OVER A FANWING IN A SUBSONIC WIND TUNNEL /
- DESIGN OF A CLOSED LOOP SUBSONIC WIND TUNNEL /
- DESIGN S CONSTRUCTION OF A SUBSONIC OPEN LOOP WIND TUNNEL /
- INVESTIGATION OF DRAG ANALYSIS OF FOUR DIFFERENT PROFILES TESTED AT SUBSONIC WIND TUNNEL
- INVESTIGATION OF DRAG ANALYSIS OF FOUR DIFFERENT PROFILES TESTED AT SUBSONIC WIND TUNNEL /
- Wind tunnels : models,aerodynamics and applications /
- DESIGN OF CAMBERED AEROFOIL FOR UNMANNED AERIAL VEHICLE BASED ON SUBSONIC WIND TUNNEL TEXT / KH. Md. Faisal Md. Faisal Kabir, Nahian Al Hossain Basunia,
Pwnc: Thesis Paper of AE in B.Sc Prog.
- 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 /
Pwnc: 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 /