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A hybrid computational aeroacoustics method is applied to investigate the effect of wavy leading edges on rod–airfoil interaction noise. The flow field is solved by an incompressible large-eddy sim... Click to show full abstract
A hybrid computational aeroacoustics method is applied to investigate the effect of wavy leading edges on rod–airfoil interaction noise. The flow field is solved by an incompressible large-eddy sim...
Keywords:
leading edges;
wavy leading;
edges rod;
interaction noise;
airfoil interaction;
rod airfoil
Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!