書誌事項
- タイトル別名
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- 254 Numerical Analysis for Aeroacoustics by using of a Finite Difference Method
抄録
Finite difference model is proposed to predict sounds induced by vortex in the wake of a body located in free stream in duct. Flow field around the body is calculated by applying a conventional scheme for incompressible fluid such as MAC scheme. To predict the aerodynamic sound, Lighthill's aeroacoustic analogy is applied. Extended Lighthill's wave equations introduced by Curie which takes into account the effect of the solid body are solved by Hancock scheme. In this study, we caluclated the flow around a elliptic cylinder in a duct to apply our scheme in a compact condition. The calculation can reproduce the propagation of dipole sound generated from the body and the reflection of one from the wall.
収録刊行物
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- 年次大会講演論文集
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年次大会講演論文集 2005.2 (0), 191-192, 2005
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
- 1390282681038714368
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- NII論文ID
- 110006190624
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- ISSN
- 24331325
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可