Eitemau Tebyg: SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF BOUNDARY VALUE PROBLEMS POLAR AND CYLINDRICAL COORDINATE SYSTEM /
- A SCALAR FUNCTION FORMULATION FOR STRESS ANALYSIS OF CYLINDRICAL PANELS /
- APPLICATION OF SCALAR FUNCTION FORMULATION TO A SEMI CIRCULAR DEEP ARCH /
- Differential equations with boundary-value problems /
- FORMULATION AND FUNCTIONAL EVALUATION OF NANOEMULSIFIED IBUPROFEN FOR ORAL DELIVERY /
- The Elements of Coordinate Geometry cartesian coordinates /
- The Elements of Coordinate Geometry : Part-1 , Cartesian Coordinates /
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.
- 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 /
- 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 /