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The document discusses three studies on active flow control techniques applied to low-pressure turbines: 1) A study of discrete sweeping jet and steady jet excitation on a wing with a simple-hinged flap at deflections of 20, 40, and 60 degrees. Sweeping jets reduced separation at lower deflections but not at 60 degrees, while both techniques increased lift but steady jets reduced lift at highest mass flows. 2) A review of active flow control applications for challenging low-pressure turbine flows like se

Author

Fahad Ali

Language

EN