書誌事項
- タイトル別名
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- Shortening of the start-up process of hybrid rocket using cavity
抄録
<p>In order to shorten the startup process of the hybrid rocket, a cavity was provided in the solid fuel and ignited in this groove to propagate the flame along the groove. By changing the aspect ratio of the groove, the temperature distribution and the velocity distribution in the groove were investigated, experimentally and numerically. From these results, the mechanism of the flame stabilization and increasing the flame propagation speed by the cavity was considered. High temperature gas generated in the cavity stayed in the vicinity of the upstream- wall, and it was effective for increasing the flame propagation speed when the aspect ratio was larger than 1.</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), OS14-7-, 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
- 1390001288139295488
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- NII論文ID
- 130007654075
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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