Experimental Validation of S809 Airfoil and Comparison of lift and drag coefficients of Owl, Seagull and S809 Airfoils.
Description
The dataset (Experimental Validation of S809 Airfoil) compares the experimental data of S809 airfoil with the data obtained from CFD analysis. The experimental data is taken from Colorado State University, and the selected Reynolds number is 500,000 at a wind speed of 7.3 m/s. This experimental data is taken from the article "Unsteady Aerodynamics Experiment Phase VI: Wind Tunnel Test Configurations and Available Data Campaigns". The CFD data is in good agreement with the experimental data. The data is present in both tabular and in graphical form. The datset (Comparison of lift and drag coefficients of Owl, Seagull and S809 Airfoils) compares the lift and drag coefficients of Owl, Seagull and S809 airfoil obtained from CFD to find out which airfoil will have higher lift to drag ratio, and hence which one can serve better when used in the design of wind turbine. The data is present in both tabular and in graphical form. Contributors: Raja Walied and Raja Moiz.