書誌事項
- タイトル別名
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- Interaction between an Oblique Shock Wave and a Circular Cylinder Placed in Supersonic Flow
- チョウオンソクリュウチュウ ニ オカレタ エンチュウ ト ナナメ ショウゲキハ
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説明
This paper presents an experimental and numerical study of interaction of an oblique shock wave and a detached shock wave formed ahead of a circular cylinder.<BR>Measurements of pressure distribution and shock shape are made on circular cylinder at free stream Mach number of 2.48 and for 27.5° shock impingement. Next, supersonic flow over a circular cylinder is computed in the plane of symmetry of the flow field. A time-dependent second-order finite difference method is used to solve the equations for a perfect gas. The shock wave is treated as a discontinuity, across which the RANKINE-HUGONIOT relations are used to compute the flow conditions behind the shock.<BR>It is shown that an upward subsonic jet is formed right below the impingement point and therefore increases the shock detachment distance.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 28 (321), 490-495, 1980
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679482005504
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- NII論文ID
- 130003958387
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 2196028
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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