Propeller wake interaction noise with downstream wing: effect of wing sweep, lean, and offset-Reference-Cited by-同舟云学术

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Propeller wake interaction noise with downstream wing: effect of wing sweep, lean, and offset

Published:2023-06-08 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2023 Forum
language:
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Author:

Akiwate Deepak C.¹,Parry Anthony¹

Affiliation:

1. University of Southampton

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3357

Reference36 articles.

1. Urban air mobility: A comprehensive review and comparative analysis with autonomous and electric ground transportation for informing future research

2. Advanced propulsion through the 1990s - An airframer's view

3. Parry, A. B. "Theoretical prediction of counter-rotating propeller noise," Ph.D. thesis,University of Leeds, 1988.

4. Ekoule, C. M. "Advanced open rotor far-field tone noise," Ph.D. thesis,University of Southampton, 2017.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Synchrophasing control of multiple propellers based on hardware in the loop experimental platform;Aerospace Science and Technology;2024-10

2. Aeroacoustics source mechanisms of fixed-wing VTOL configuration;AIAA AVIATION 2023 Forum;2023-06-08

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