An Aeroacoustic Study of Full-Scale and Small-Scale Generic Landing Gear Models with Identical Geometry
Author:
Affiliation:
1. Central Aerohydrodynamic Institute (TsAGI), 105005 Moscow, Russia
2. China Aerodynamics Research and Development Center, Mianyang 621000, China
Abstract
Funder
Ministry of Science and Higher Education of the Russian Federation
Publisher
MDPI AG
Subject
Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science
Link
https://www.mdpi.com/2076-3417/13/4/2295/pdf
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3. Noise Reduction Technologies for Aircraft Landing Gear—A Bibliographic Review;Zhao;Prog. Aerosp. Sci.,2020
4. Sound radiation from aircraft Wheel-Well/Landing-Gear configurations;Heller;J. Aircr.,1977
5. Hayes, J., Horne, W., Soderman, P., and Bent, P. (1997, January 12–14). Airframe Noise Characteristics of a 4.7 Percent Scale DC-10 Model. Proceedings of the 3rd AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, USA.
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