Analysis of the Sound Field Structure in the Cabin of the RRJ-95NEW-100 Prototype Aircraft-Reference-Cited by-同舟云学术

Analysis of the Sound Field Structure in the Cabin of the RRJ-95NEW-100 Prototype Aircraft

Published:2023-06-14 Issue:6 Volume:10 Page:559
ISSN:2226-4310
Container-title:Aerospace
language:en
Short-container-title:Aerospace

Author:

Lavrov Vladimir¹,Moshkov Petr²,Strelets Dmitry²^ORCID

Affiliation:

1. IRKUT Corporation Regional Aircraft, Moscow 115280, Russia

2. Moscow Aviation Institute (National Research University), Moscow 125993, Russia

Abstract

The results of in-flight experiments to determine the structure of the sound field in the cabin and pressure fluctuation fields on the surface of the fuselage of the RRJ-95NEW-100 prototype aircraft are presented here. Wall pressure fluctuation spectrums are obtained for three zones of measuring windows (forward, center, and rear fuselage) in cruising flight mode. The effect of the jet on the pressure fluctuation levels in the tail fuselage is considered. For an aircraft without an interior, the contribution of the main sources to the total intensity calculated through A-weighted overall sound pressure levels is determined. It has been determined that the main noise sources in the cabin of the RRJ-95NEW-100 prototype aircraft in cruising flight mode are pressure fluctuation fields on the fuselage surface (turbulent boundary layer noise) and the air conditioning system. The ratio between the sources varies along the length of the cabin.

Publisher

MDPI AG

Subject

Aerospace Engineering

Link

https://www.mdpi.com/2226-4310/10/6/559/pdf

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