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Reduction of rotorcraft BVI using synthetic jets; computational studies using LES
Marcel Ilie
Mechanical Engineering
Georgia Southern University
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peer-review
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Dive into the research topics of 'Reduction of rotorcraft BVI using synthetic jets; computational studies using LES'. Together they form a unique fingerprint.
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Engineering
Blade Vortex Interaction
100%
Rotorcraft
100%
Aerodynamic Coefficient
25%
Leading Edge
25%
Reynolds' Number
12%
Vortex
12%
Airfoil
12%
Aerodynamic Performance
12%
Main Source
12%
Free Stream Velocity
12%
Core Size
12%
Interaction Effect
12%
Main Idea
12%
Aerodynamic Stability
12%
Scale Model
12%