推進薬タンクを対象とした微小重力下横スロッシング挙動に関する研究
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DOI[10.15011//jasma.36.360403]のデータに遷移します
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- 資料種別
- 記事
- 著者・編者
- 道原孟里今井良二
- 出版年月日等
- 2019-10-31
- 出版年(W3CDTF)
- 2019-10-31
- 並列タイトル等
- Study on the lateral sloshing behavior under microgravity condition targeted for a propellant tank
- タイトル(掲載誌)
- International journal of microgravity science and application : IJMSA
- 巻号年月日等(掲載誌)
- 36(4)
- 掲載巻
- 36(4)
- ISSN(掲載誌)
- 2188-9783
- ISSN-L(掲載誌)
- 0915-3616
- 本文の言語コード
- jpn
- DOI
- 10.15011//jasma.36.360403
- 国立国会図書館永続的識別子
- info:ndljp/pid/11488733
- コレクション(共通)
- コレクション(障害者向け資料:レベル1)
- コレクション(個別)
- 国立国会図書館デジタルコレクション > 電子書籍・電子雑誌 > 学術機関 > 学協会
- 収集根拠
- オンライン資料収集制度
- 受理日(W3CDTF)
- 2020-05-14T20:27:18+09:00
- 保存日(W3CDTF)
- 2020-05-14
- 記録形式(IMT)
- application/pdf
- オンライン閲覧公開範囲
- 国立国会図書館内限定公開
- デジタル化資料送信
- 図書館・個人送信対象外
- 遠隔複写可否(NDL)
- 可
- 掲載誌(国立国会図書館永続的識別子)
- info:ndljp/pid/11488728
- 連携機関・データベース
- 国立国会図書館 : 国立国会図書館デジタルコレクション
- 要約等
- Fluid behavior in microgravity (µg) is different from in ground gravity since surface tension and wetting are dominant in µg conditions. In propellant tanks for artificial satellites and future on-orbit spacecraft, sloshing due to disturbance and settling behavior from changes in acceleration have to be understood for the design of the propellant supply system and attitude control system. In this paper, we observed sloshing behaviors in cylindrical containers in µg conditions created by a drop tower facility. In order to investigate the effects of the contact line velocity on dynamic contact angle, we measured dynamic contact angle using a capillary tube. CFD analysis introducing Cox’s equation in consideration of capillary experimental results were also conducted and these results were compared with µg experimental results. Regarding the experimental results, the diameter of the test tank, excitation acceleration, and kinematic viscosity were found to have a significant effect on sloshing behavior in a µg condition. Regarding the comparison between the CFD analysis results and the experimental results, there was a slight difference in the wave shape and the time required for the liquid to reach the top of the test tank. Conversely, there was a qualitative agreement between the fluctuation period and the approximate shape of the liquid surface over time.
- DOI
- 10.15011//jasma.36.360403
- オンライン閲覧公開範囲
- インターネット公開
- 連携機関・データベース
- 科学技術振興機構 : J-STAGE
- 要約等
- Fluid behavior in microgravity (µg) is different from in ground gravity since surface tension and wetting are dominant in µg conditions. In propellant tanks for artificial satellites and future on-orbit spacecraft, sloshing due to disturbance and settling behavior from changes in acceleration have to be understood for the design of the propellant supply system and attitude control system. In this paper, we observed sloshing behaviors in cylindrical containers in µg conditions created by a drop tower facility. In order to investigate the effects of the contact line velocity on dynamic contact angle, we measured dynamic contact angle using a capillary tube. CFD analysis introducing Cox’s equation in consideration of capillary experimental results were also conducted and these results were compared with µg experimental results. Regarding the experimental results, the diameter of the test tank, excitation acceleration, and kinematic viscosity were found to have a significant effect on sloshing behavior in a µg condition. Regarding the comparison between the CFD analysis results and the experimental results, there was a slight difference in the wave shape and the time required for the liquid to reach the top of the test tank. Conversely, there was a qualitative agreement between the fluctuation period and the approximate shape of the liquid surface over time.
- DOI
- 10.15011//jasma.36.360403
- オンライン閲覧公開範囲
- インターネット公開
- 関連情報(URI)
- 連携機関・データベース
- 国立情報学研究所 : CiNii Research
- 提供元機関・データベース
- Japan Link Center学術機関リポジトリデータベース雑誌記事索引データベースCiNii Articles
- 書誌ID(NDLBibID)
- 11488733
- NII論文ID
- 130007739893