Symmetric airfoil geometry effects on leading edge noise
Computational aeroacoustic methods are applied to the modeling of noise due to interactions between gusts and the leading edge of real symmetric airfoils. Single frequency harmonic gusts are interacted with various airfoil geometries at zero angle of attack. The effects of airfoil thickness and lead...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
2013-10.
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| Subjects: | |
| Online Access: | Get fulltext |