Experimental Investigation of Helicopter Noise While Approaching an Elevated Helipad

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
G. Gibertini, Silvano Rezzonico, Marco Rossetti, A. Zanotti
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引用次数: 0

Abstract

The present paper describes a test campaign performed to investigate the noise footprint emitted by a helicopter in an idealised urban context, reproducing the approach to an elevated helipad. The test campaign was performed in Politecnico di Milano’s anechoic chamber and was finalised to investigate the effects produced only by helicopter noise. The set up consisted of a two-blade main rotor helicopter model and an aluminium rectangular prism model reproducing the landing building. Ground observer perceptions were recorded by means of a surface microphone and a realistic landing trajectory was approximated as a succession of fixed point measurements. Collected data were analysed through acoustic spectra and sound maps. Spectra were used to comprehend physical phenomena, such as reflection, diffraction and shielding, and to analyse the different contributions of helicopter noise. A sound map analysis enabled us to obtain a global perspective of the involved phenomena and to understand th extent to which people close to a building are stressed by a helicopter approaching an elevated urban helipad. Moreover, the experimental database, obtained over a free geometry, can be considered a useful tool for the validation of aeroacoustic solvers with different levels of fidelity.
直升机接近高架停机坪时噪声的实验研究
本文描述了一项测试活动,以调查直升机在理想的城市环境中发出的噪音足迹,再现了直升飞机到达高架停机坪的方法。测试活动是在米兰理工大学的消声室进行的,并最终调查了仅由直升机噪音产生的影响。该装置由一个双叶片主旋翼直升机模型和一个再现着陆大楼的铝矩形棱镜模型组成。利用地面麦克风记录地面观测者的感知,并将真实的着陆轨迹近似为一系列定点测量。收集到的数据通过声谱和声图进行分析。光谱用于理解反射、衍射和屏蔽等物理现象,并分析直升机噪声的不同贡献。声音地图分析使我们能够获得有关现象的全球视角,并了解靠近建筑物的人在直升机接近高架城市直升机停机坪时受到的压力程度。此外,在自由几何上获得的实验数据库可以被认为是验证具有不同保真度水平的气动声学求解器的有用工具。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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