Research Article

Study on Dynamic Stall Control of Rotor Airfoil Based on Coflow Jet

Table 1

The variation of the peak values of the lift and moment coefficients of the airfoil with different values of


Baseline2.1728ā€”-0.4256ā€”
2.635921.31%-0.0635-85.07%
2.993437.77%-0.0215-94.95%
2.724125.37%-0.0536-87.41%
2.750226.57%-0.0506-88.11%