Experimental Investigation of Reynolds Number Scaling on the Aeroacoustics of a Simple Landing Gear Wheel-Reference-Cited by-同舟云学术

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Experimental Investigation of Reynolds Number Scaling on the Aeroacoustics of a Simple Landing Gear Wheel

Published:2024-05-30 Issue: Volume:76 Page:
ISSN:
Container-title:30th AIAA/CEAS Aeroacoustics Conference (2024)
language:
Short-container-title:

Author:

Ivanova Zoya¹,Angland David¹,Scotto Aline²

Affiliation:

1. University of Southampton

2. Airbus SAS

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3171

Reference16 articles.

1. Hubbard, H. H. ``Aeroacoustics of Flight Vehicles: Theory and Practice Volume 1: Noise Sources,'' Tech. Rep. 90-3052, NASAReferencePublication1258,1991. URL https://ntrs.nasa.gov/citations/19920001380.

2. Guo, Y. P. ``Empirical Prediction of Aircraft Landing Gear Noise,'' Tech. Rep. 2005-213780, Nasa STI, 2005. https: //doi.org/10.2514/6.2004-2888.

3. Noise Component Method for Airframe Noise

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