Experimental study of flow measurement in stunted Busemann intakes using ballistic range
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- OHTANI Kiyonobu
- Tohoku University
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- OGAWA Toshihiro
- Tohoku University
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- Ogawa Hideaki
- Royal Melbourne Institute of Technology
Bibliographic Information
- Other Title
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- 軸対称Busemann形状空気吸込み口流れ場計測のための弾道飛行装置実験
Abstract
<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>
Journal
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- The Proceedings of the Fluids engineering conference
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The Proceedings of the Fluids engineering conference 2018 (0), OS9-6-, 2018
The Japan Society of Mechanical Engineers
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Details 詳細情報について
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- CRID
- 1390564238093963520
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- NII Article ID
- 130007654312
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- ISSN
- 24242896
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed