書誌事項
- タイトル別名
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- 1012 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. Flowfield 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 curle which takes into account the effect of the solid body are solved by Hancock scheme. The calculation can reproduce the propagation of dipole sound generated from the body surface.
収録刊行物
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- 関西支部講演会講演論文集
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関西支部講演会講演論文集 2005.80 (0), _10-23_-_10-24_, 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
- 1390001205848948352
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- NII論文ID
- 110006187525
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- ISSN
- 24242756
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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