WS4-5 空力音の計測
スポンサーリンク
概要
- 論文の詳細を見る
In this report, measurement technique and experimental apparatus for aeroacoustic experiments is explained, focusing on the simultaneous measurement of flow and sound field. In order to understand the generation mechanism of aerodynamic sound, spectrum analysis and sound source identification method of aerodynamic sound are shown by experimental results of the aerodynamic sound radiated from a circular cylinder. The results show that the separating shear layer and its correlation length play an important role in generating aerodynamic sound. Therefore, unsteady motion of separated shear layer is the most important factor in controlling aerodynamic sound. The example of aerodynamic sound control is also shown.
- 一般社団法人日本機械学会の論文
- 2000-09-08
著者
関連論文
- 2次元翼から発生する空力音の計測
- 低騒音パンタグラフカバーの開発
- 音源寄与率解析を用いた騒音予測方法とその精度検証
- WS4-5 空力音の計測
- A133 二次元翼から発生する空力音の数値解析
- 後流静圧変動と空力音の相関計測
- 静圧変動計測による空力音源解析