Increasing the amplitude of Gaussian wakes entering a T106A turbine cascade delays boundary-layer separation, shrinks separated-flow regions, and reduces skin friction drag by about 50% at the highest amplitude tested.
Sengupta, Numerical lnvestigation of disturbance environments in low pressure turbines, Ph.D
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Effect of Gaussian wake amplitude on wake-induced transition for a T106A low pressure turbine cascade
Increasing the amplitude of Gaussian wakes entering a T106A turbine cascade delays boundary-layer separation, shrinks separated-flow regions, and reduces skin friction drag by about 50% at the highest amplitude tested.