書誌事項
- タイトル別名
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- Experimental study of flow measurement in stunted Busemann intakes using ballistic range
抄録
<p>This paper reports a preliminary experimental result of a supersonic free-flight ring-shape model for understanding of flow field in stunted Busemann intakes by using ballistic range at Institute of Fluid Science, Tohoku University. The ring-shape model is launched by the ballistic range. The flow field around a supersonic free-flight ring-shaped model is visualized by shadowgraph method, and recorded by a high-speed camera. The ring-shaped model is separated from the sabot, shock wave is generated thorough a supersonic free-flight ring-shaped model.</p>
収録刊行物
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- 流体工学部門講演会講演論文集
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流体工学部門講演会講演論文集 2018 (0), OS9-6-, 2018
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
- 1390564238093963520
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- NII論文ID
- 130007654312
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- ISSN
- 24242896
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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