The aim of the study is to optimize a wing section which can have an ability to operate at
higher aerodynamic efficiency and function as a high lifting device. The computational study …

The main objective of the present work is to find a method increases the efficiency of the
airfoil that is used for blade in wind turbine, wing in aircraft, propeller and helicopter (like …

Problems associated with high angle of attack (AoA) airfoil are flow separation, stalling, high
drag and low lift-to-drag ratio (CL/CD). Therefore it demands for research to develop a better …

The present study aimed to design a subsonic wind tunnel and compare the numerical and
experimental results to ensure the accuracy of the design that has been manufactured after …

The aim of this study is to find the optimal location and area of exit for the boundary layer
suction control parameter. A computational study is carried over a finite wing section to …

In this study, a numerical and experimental investigation for the flow separation over 170
mm chord, the NREL S822 aerofoil low Reynolds number wind turbine blade aerofoil …

The possibility of decreasing the drag coefficient of the slotted airfoil is investigated at
Reynold number 1.6 x10 for the angles of attack were ranged from 0 to 20. For this purpose …

The majority of wind turbine models are built to work in areas with high wind speeds. Such
turbines would waste a lot of the energy available in low-speed zones. The performance of …

Designing an aircraft flying at high angle of attack (AoA) is an interest to aerospace
community. Problems associated with high AoA is flow separation, stalling, high drag and …

Wind energy is one of the most promising alternative energy sources for the continuously
increasing demand for worlds' energy consumption. In recent decades, there has been a …