Effect of sweep angle and of wall-pressure statistics on the free-field directivity of airfoil trailing-edge noise-Reference-Cited by-同舟云学术

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Effect of sweep angle and of wall-pressure statistics on the free-field directivity of airfoil trailing-edge noise

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Grasso Gabriele¹,Roger Michel¹,Moreau Stéphane²

Affiliation:

1. École Centrale de Lyon

2. University of Sherbrooke

Publisher

American Institute of Aeronautics and Astronautics

Reference40 articles.

1. Envia,E.,andKerschen,E.J.“InfluenceofVaneSweeponRotor-StatorInteractionNoise,”Tech.rep.,NASA,1990.

2. Envia,E.,andNallasamy,M.“DesignSelectionandAnalysisofaSweptandLeanedStatorConcept,”Tech.rep.,NASA,1998.

3. Prediction of tonal ducted fan noise

4. Benefits of Swept-and-Leaned Stators for Fan Noise Reduction

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4. A parametric study of serration design for trailing–edge broadband noise reduction;Applied Acoustics;2023-08

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