書誌事項
- タイトル別名
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- Numerical analysis for transonic cascade flows using the AF2 scheme.
- AF2ホウ ニ ヨル センオンソク ヨクレツカン ナガレ ノ スウチ カイセキ
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抄録
An approximate factorization scheme has been developed for analyzing transonic cascade flows. In this scheme, upwind differencing is used for introducing artificial viscosity in the supersonic region, and central differencing in the subsonic region. The resulting simple two- and three-banded matrices are solved by the relaxation procedure. In this paper, the efficiency of this scheme is demonstrated by solving the channel flow problem, and then this scheme is applied to some transonic cascade flows. The results are in good agreement with those obtained by other methods.
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 52 (475), 1184-1190, 1986
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
- 1390001206183581952
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- NII論文ID
- 110002400246
- 130004217631
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- NII書誌ID
- AN00187441
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- ISSN
- 18848346
- 03875016
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- NDL書誌ID
- 3063677
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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
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可