摘要
介绍用有机玻璃制作的两套结构尺寸不同的微穿孔消声声衬试件,在单级跨音压气机台上进行的3次降噪实验。目前国内尚无人获得微穿孔消声声衬在跨音、大流量、高声压级模拟声源环境条件下的噪声测试数据。通过实验,为进一步合理地设计声衬提供了参考数据,并看到了这种降噪方法在流体机械管道消声方面的应用前景。
Some experimental results and analyses from the measurements of the sound field in a single transonic axial compressorr inlet duct with single plastic glass lining are presented.The plastic glass linings are designed and made by ourselves (two kinds of perforate rating,σ 1=2 85% and σ 2=5 85%).The experimental results are firstly obtained in China from the real sonic fields in a single transonic axial compressor at high sound pressure conditions (>150dB).The experimental results and conclusions provide some reference for the further investigation on design of the acoustic treatment assemblies in aeroengine nacells and turbomachinery duct.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1994年第3期315-317,共3页
Journal of Aerospace Power
关键词
穿孔吸声衬
噪声控制
飞机
Perforated linigs Noise control Noise reduction systems