Aerodynamic and Aeroacoustic Study of Low Reynolds Number Rotors: Influence of Pitch Angle, Airfoil Camber and Thickness-Reference-Cited by-同舟云学术

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Aerodynamic and Aeroacoustic Study of Low Reynolds Number Rotors: Influence of Pitch Angle, Airfoil Camber and Thickness

Published:2022-06-13 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA/CEAS Aeroacoustics 2022 Conference
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Author:

Li Volsi Pietro¹,Jardin Thierry²,Gojon Romain²,Gomez-Ariza David³,Moschetta Jean-Marc²,Parisot-Dupuis Hélène²,Brogna Gianluigi¹

Affiliation:

1. Parrot SA

2. ISAE-SUPAERO

3. SENSEFLY

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3109

Reference35 articles.

1. Serré, R., Gourdain, N., Jardin, T., Delattre, G., and Moschetta, J. M. “Analysis of the flow produced by a low-Reynolds rotor optimized for low noise applications. Part II: Acoustics,” 43rdEuropean Rotorcraft Forum, ERF 2017, Vol.2, 2017, pp.799-805.

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1. Analysis of MAV Rotors Optimized for Low Noise and Aerodynamic Efficiency with Operational Constraints;Fluids;2024-04-19

2. Acoustic Liners Integrated in Rotor Blades of Unmanned Air Vehicles;AIAA AVIATION 2023 Forum;2023-06-08

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