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Sound Generation in Compressible Mixing Layers

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Sound Generation in Compressible Mixing Layers

国立国会図書館請求記号
Z53-Y271
国立国会図書館書誌ID
5978490
資料種別
記事
著者
Ye Liほか
出版者
Tokyo : Japan Society of Mechanical Engineers
出版年
2001-11
資料形態
掲載誌名
JSME international journal. Ser. B, Fluids and thermal engineering 44(4) 2001.11
掲載ページ
p.505~512
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資料種別
記事
著者・編者
Ye Li
Mamoru Tanahashi
Toshio Miyauchi
タイトル(掲載誌)
JSME international journal. Ser. B, Fluids and thermal engineering
巻号年月日等(掲載誌)
44(4) 2001.11
掲載巻
44
掲載号
4
掲載ページ
505~512
掲載年月日(W3CDTF)
2001-11
ISSN(掲載誌)
1340-8054
ISSN-L(掲載誌)
1340-8054
出版事項(掲載誌)
Tokyo : Japan Society of Mechanical Engineers
出版地(国名コード)
JP
本文の言語コード
eng
NDLC
対象利用者
一般
所蔵機関
国立国会図書館
請求記号
Z53-Y271
連携機関・データベース
国立国会図書館 : 国立国会図書館雑誌記事索引
書誌ID(NDLBibID)
5978490
整理区分コード
632

デジタル

要約等
Direct numerical simulations have been performed to clarify the sound generation mechanism in a two-dimensional temporally evolving compressible mixing layers. The sound generation in mixing layer is governed by the variations of vorticity which are induced by the Kelvin-Helmholtz instability. The pressure fluctuations with high frequency are observed in the period of vortex roll-up, and the amplitude of pressure fluctuations increase on the occasion of vortex pairing. The acoustic source term is governed by the Reynolds stress component and the viscous component is negligible. The effects of convective Mach number Mc on sound generation are also investigated. Both the pressure fluctuations and acoustic source term increase with the increase of convective Mach number. For Mc=0.6, shock wave called'eddy shocklet, is produced by the vortex pairing, which dominates the sound generation from the mixing layer at high Mc. The far-field sound computed by DNS is compared with the predictions based on the acoustic analogies derived by Powell and Lighthill. The prediction by Powell's analogy shows a good agreement with DNS, while the pressure fluctuations predicted by Lighthill's analogy are low compared with the DNS results after the vortex pairing.
DOI
10.1299/kikaib.66.646_1527
オンライン閲覧公開範囲
インターネット公開
連携機関・データベース
科学技術振興機構 : J-STAGE

デジタル

要約等
Direct numerical simulations have been performed to clarify the sound generation mechanism in a two-dimensional temporally evolving compressible mixing layers. The sound generation in mixing layer is governed by the variations of vorticity which are induced by the Kelvin-Helmholtz instability. The pressure fluctuations with high frequency are observed in the period of vortex roll-up, and the amplitude of pressure fluctuations increase on the occasion of vortex pairing. The acoustic source term is governed by the Reynolds stress component and the viscous component is negligible. The effects of convective Mach number Mc on sound generation are also investigated. Both the pressure fluctuations and acoustic source term increase with the increase of convective Mach number. For Mc=0.6, shock wave called'eddy shocklet, is produced by the vortex pairing, which dominates the sound generation from the mixing layer at high Mc. The far-field sound computed by DNS is compared with the predictions based on the acoustic analogies derived by Powell and Lighthill. The prediction by Powell's analogy shows a good agreement with DNS, while the pressure fluctuations predicted by Lighthill's analogy are low compared with the DNS results after the vortex pairing.
オンライン閲覧公開範囲
インターネット公開
関連情報
Sound Generation in Compressible Mixing Layers
Sound Generation in Compressible Mixing Layers
参照
Sound generation in a mixing layer
Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute
Radiation boundary conditions for acoustic and elastic wave calculations
The generation of sound by aerodynamic sources in an inhomogeneous steady flow
Boundary conditions for direct simulations of compressible viscous flows
The compressible turbulent shear layer: an experimental study
On sound generated aerodynamically I. General theory
Theory of Vortex Sound
Why Do Vortices Generate Sound?
Direct computation of the sound from a compressible co-rotating vortex pair
The scattering of sound waves by a vortex: numerical simulations and analytical solutions
連携機関・データベース
国立情報学研究所 : CiNii Research
提供元機関・データベース
Japan Link Center
Japan Link Center
雑誌記事索引データベース
Crossref
Crossref
CiNii Articles
CiNii Articles
学術機関リポジトリデータベース
学術機関リポジトリデータベース
書誌ID(NDLBibID)
5978490
NII論文ID
110003474278
130004223916