首页> 外国专利> MODELING METHOD OF ACOUSTIC SOURCE OF JET NOISE, ANALYSIS METHOD OF JET NOISE, AND DESIGN METHOD OF AIRCRAFT

MODELING METHOD OF ACOUSTIC SOURCE OF JET NOISE, ANALYSIS METHOD OF JET NOISE, AND DESIGN METHOD OF AIRCRAFT

机译:喷气噪声的声源建模方法,喷气噪声的分析方法以及飞机的设计方法

摘要

PROBLEM TO BE SOLVED: To provide a modeling method of acoustic sources of jet noise and an analysis method of jet noise and a design method of aircraft therewith.;SOLUTION: An intensity distribution is determined from stationary RANS analysis for stream from jet engines and, following its discretization, each acoustic source intensity is obtained by setting a plurality of point acoustic sources. Furthermore. based on the noise level of observation points of far acoustic field utilizing existing databases, the phase of each point acoustic source is optimized and determined. Thus, an acoustic source model containing a plurality of point acoustic sources specified with the acoustic source intensity and the phase. By analyzing the acoustic field near stream of jet engine using the present acoustic source model, jet noise can be analyzed and, based on the analytical result, an aircraft is designed with an airframe capable of insulating noise.;COPYRIGHT: (C)2008,JPO&INPIT
机译:要解决的问题:提供一种喷气噪声的声源建模方法,一种喷气噪声分析方法以及一种飞机的设计方法。解决方案:通过对喷气发动机流进行静态RANS分析确定强度分布,并且离散化之后,通过设置多个点声源来获得每个声源强度。此外。基于现有数据库的远场观测点噪声水平,优化确定每个点声源的相位。因此,声源模型包含由声源强度和相位指定的多个点声源。通过使用当前声源模型分析喷气发动机近流的声场,可以分析喷气噪声,并根据分析结果设计出一种飞机,飞机的机体具有绝缘的噪声。版权所有:(C)2008,日本特许厅

著录项

  • 公开/公告号JP2008102095A

    专利类型

  • 公开/公告日2008-05-01

    原文格式PDF

  • 申请/专利权人 KAWASAKI HEAVY IND LTD;

    申请/专利号JP20060286819

  • 申请日2006-10-20

  • 分类号G01H3/00;B64F5/00;

  • 国家 JP

  • 入库时间 2022-08-21 20:21:23

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