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- 井藤 創
- 防衛大学校
書誌事項
- タイトル別名
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- Visualization of Velocity Fields around Hypersonic Compression Corner Flows
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Understanding of hypersonic viscous interaction phenomenon over control surfaces and engine intakes is of particular importance for designers of hypersonic vehicles. However, experimental data of velocity fields around the compression corner which is an idealized configuration of these practical situations are sparse chiefly because it is difficult to obtain such data owing to short duration, high velocity, and rarefaction of the test flow in hypersonic ground facilities. In this report, we shall try to apply the high frequency impulsive glow discharge technique to obtaining the hypersonic velocity fields. The experiment is carried out in a hypersonic gun tunnel at Mach number 10 and Reynolds number based on the frontal plate chord length 2.8×105. Time lines are obtained successfully, even for separated flow cases.
収録刊行物
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- 可視化情報学会誌
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可視化情報学会誌 24 (Supplement2), 83-84, 2004
社団法人 可視化情報学会
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詳細情報 詳細情報について
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- CRID
- 1390001204619699456
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- NII論文ID
- 10013560006
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- NII書誌ID
- AA11907562
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- ISSN
- 1884037X
- 09164731
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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