Acoustic Assessment of BLI Effects on Airbus Nautilius Engine Integration Concept - Part II: Noise Radiation-Reference-Cited by-同舟云学术

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Acoustic Assessment of BLI Effects on Airbus Nautilius Engine Integration Concept - Part II: Noise Radiation

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

Lorteau Mathieu¹,Le Garrec Thomas¹,Daroukh Majd¹,Polacsek Cyril¹

Affiliation:

1. Office National d'Etudes et de Recherches Aerospatiales

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2992

Reference25 articles.

1. Rogero, J.M., Negulescu, C., Faure, R., and Airbus-Operation-SAS, "Ensemble pour aéronef comprenant des moteurs à propulsionparingestiondelacouchelimite,"PatentFR3052743BI,2016.

2. Negulescu, C., Rogero, J.M., Faure, R., and Airbus-Operation-SAS, "Assembly for aircraft comprising engines with boundary layerpropulsionbyinjection,"PatentUS2017/0361939AI,2017.

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1. Open Fan Noise Confinement Effects in a Closed Wind-Tunnel: Numerical Methodology and Evaluation;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Turbomachinery Noise Review;International Journal of Turbomachinery, Propulsion and Power;2024-03-13

3. Acoustic Assessment of BLI Effects on Airbus Nautilius Engine Integration Concept - Part I: Noise Generation;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13

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