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跨声速风洞试验段低噪声壁板模型的声学试验

谷嘉锦

空气动力学学报2001,Vol.19Issue(1):62-65,4.
空气动力学学报2001,Vol.19Issue(1):62-65,4.

跨声速风洞试验段低噪声壁板模型的声学试验

Acoustical experiment of low noise wall models for testing section in transonic wind tunnels

谷嘉锦1

作者信息

  • 1. 南京航空航天大学,
  • 折叠

摘要

Abstract

Acoustical Experiment of Low noise Wall models for testingsection in transonic Wind tunnels is introduced in this paper. The Experimental results are provided to show that: (1) edgetone generated by slanted hole configuration is main sound source, (2) Screen and spllitter-plates successfully suppress the edgetone, (3) The design way in refer ence[1] for low noise wall is very useful.

关键词

风洞/边缘音/噪声控制

分类

航空航天

引用本文复制引用

谷嘉锦..跨声速风洞试验段低噪声壁板模型的声学试验[J].空气动力学学报,2001,19(1):62-65,4.

空气动力学学报

OA北大核心CSCD

0258-1825

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