Noise Control Technology for the Airplane

M. Hirai
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引用次数: 1

Abstract

In Japan, a 5-year R&D project has been in progress toward the development of an environment friendly high performance regional jet aircraft under auspice from New Energy Development Organization of Japan (NEDO) since 2003. In the project, the research of airframe noise has been conducted for achieving lower commercial noise.At first experiments were conducted on 20%-scale half span model in the JAXA Wind Tunnel from 2005 to 2006. In the test, the array microphone has been used to visualize the airframe sound source and it was found that the slat noise is the one of the biggest sound source for the aircraft approach condition. Then the generation mechanism of the slat noise has been calculated by using CFD for developing the device that was able to reduce the slat noise.
飞机噪声控制技术
在日本,自2003年以来,在日本新能源开发组织(NEDO)的支持下,一项为期5年的研发项目一直在进行,旨在开发环保型高性能支线喷气式飞机。本项目对机体噪声进行了研究,以达到降低商用噪声的目的。从2005年到2006年,在JAXA风洞中进行了20%比例的半跨度模型实验。在试验中,采用阵列传声器对机体声源进行可视化,发现板条噪声是飞机进近时最大的声源之一。在此基础上,利用CFD计算了板条噪声的产生机理,研制了降低板条噪声的装置。
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