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The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is investigated. The three components of the velocity at the aerodynamic interface… Click to show full abstract
The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is investigated. The three components of the velocity at the aerodynamic interface plane were measu...
Keywords:
control study;
flow control;
duct using;
passive flow;
study duct;
duct
Journal Title: AIAA Journal
Year Published: 2017
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2017
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!