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

被引:0
|
作者
Lavrov, Vladimir [1 ]
Moshkov, Petr [2 ]
Strelets, Dmitry [2 ]
机构
[1] IRKUT Corp Reg Aircraft, Moscow 115280, Russia
[2] Natl Res Univ, Moscow Aviat Inst, Moscow 125993, Russia
关键词
aircraft; pressure fluctuations; cabin noise; RRJ-96NEW-100; aeroacoustics; WALL PRESSURE-FLUCTUATIONS; MODEL PREDICTIONS; ENGINE NOISE; WINGS;
D O I
10.3390/aerospace10060559
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.
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页数:13
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