Boundary Layer Separation Control With Fluidic Oscillators

By C. Cerretelli, K. Kirtley. 2009

137 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/d022dc4f1cdf9bdca0706fdbcebc7ef636ff49b0

Citations in the corpus

• Performance Enhancement of a Vertical Tail Model with Sweeping Jet Actuators (2013, unknown): “In some of those designs [2 - 4] a wedge was placed in the center of the exit nozzle to ensure that the resulting oscillatory jet dwells at two prescribed angles.”