Framework for Multi-Fidelity Assessment of Open Rotor Propeller Aeroacoustics-Reference-Cited by-同舟云学术

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Framework for Multi-Fidelity Assessment of Open Rotor Propeller Aeroacoustics

Published:2024-05-30 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA/CEAS Aeroacoustics Conference (2024)
language:
Short-container-title:

Author:

Huang Guangyuan¹,Sharma Ankit¹,Chen Xin¹,Riaz Atif¹,Jefferson-Loveday Richard²

Affiliation:

1. Cranfield University Cranfield School of Aerospace Transport and Manufacturing

2. King's College London

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3098

Reference23 articles.

1. [1]Guynn,MarkD.,JeffreyJ.Berton,WilliamJ.Haller,EricS.Hendricks,andMichaelT.Tong. Performanceandenvironmental assessment of anadvanced aircraftwith open rotorpropulsion.No.L-20189.2012.

2. [2]Airbus,"GMF2023-2042Presentation,"[onlinepresentation],URL:https://www.airbus.com/sites/g/files/jlcbta136/files/2023-06/GMF%202023-202042%20Infographic_0.pdf [retrieved 8 December 2023].

3. Modeling aerodynamically generated sound of helicopter rotors

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