書誌事項
- タイトル別名
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- A Study on Behaviour of Vortex and Shock in Transonic Pulsating Jet. Phenomena in Flow Process with Increase in Jet Velocity.
- センオンソク ミャクドウ フンリュウ ニ オケル ウズ ト ショウゲキハ ノ キョドウ ニ カンスル ケンキュウ ゾウソクカテイ ニ オケル ナガレバ ノ ゲンショウ
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抄録
Noise radiates from a jet issuing from an exhaust pipe of automotive engines and reciprocating compressors. The jet is unsteady and has some sources of noise such as the jet itself, shock wave and the interaction between shock and vortex, between shock and shock, between shock and jet boundary, etc. In order to analyze the mechanism of noise generation, in particular the noise caused by the shock-vortex interaction, the pulsating jet from the exhaust pipe is numerically simulated. A Random-Choise Method was employed for the calculation of the flow field in the pipe and a TVD scheme for the flow field downstream of the pipe end. The flow fields with the pulsation at the different frequencies were examined. As a result, the relation between the structure of the unsteady jet and the noise generation was, in part, clarified.
収録刊行物
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- 日本機械学会論文集B編
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日本機械学会論文集B編 69 (677), 45-52, 2003
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001206184262144
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- NII論文ID
- 130004224774
- 110002387766
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- NII書誌ID
- AN00187441
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- ISSN
- 18848346
- 03875016
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- NDL書誌ID
- 6446100
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可