Experimental Study of the Effect of Boundary-Layer Transition on Rotor Aeroacoustics-Reference-Cited by-同舟云学术

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Experimental Study of the Effect of Boundary-Layer Transition on Rotor Aeroacoustics

Published:2024-05 Issue:5 Volume:62 Page:1974-1981
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Li Xiangtian¹^ORCID,Wu Han¹^ORCID,Li Yuhong¹^ORCID,Zhou Peng¹,Zhong Siyang²,Zhang Xin¹^ORCID,Ma Zhaokai³

Affiliation:

1. Hong Kong University of Science and Technology, Clear Water Bay, Kowloon, Hong Kong, People’s Republic of China

2. Hong Kong Polytechnic University, Hung Hom, Kowloon, Hong Kong, People’s Republic of China

3. Nanjing University of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China

Funder

RGC

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J063785

Reference34 articles.

1. RizziS. A.HuffD. L.BoydD. D.BentP.HendersonB. S.PascioniK. A.SargentD. C.JosephsonD. L.MarsanM.HeH. B.et al. “Urban Air Mobility Noise: Current Practice, Gaps, and Recommendations,” NASA TP-2020-50074337, 2020.

2. Air taxi service for urban mobility: A critical review of recent developments, future challenges, and opportunities

3. Aeroacoustic Investigation of a Propeller Operating at Low Reynolds Numbers

4. Laminar Separation Bubble Noise on a Propeller Operating at Low Reynolds Numbers

5. Performance and noise prediction of low-Reynolds number propellers using the Lattice-Boltzmann method

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