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Volume number36 (4)
推進薬タンクを対象と...

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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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

Persistent ID (NDL)
info:ndljp/pid/11488733
Material type
記事
Author
道原孟里ほか
Publisher
日本マイクログラビティ応用学会
Publication date
2019-10-31
Material Format
Digital
Journal name
International journal of microgravity science and application : IJMSA 36(4)
Publication Page
-
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Summary, etc.:

Fluid behavior in microgravity (µg) is different from in ground gravity since surface tension and wetting are dominant in µg conditions. In propellant...

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Digital

Material Type
記事
Author/Editor
道原孟里
今井良二
Publication Date
2019-10-31
Publication Date (W3CDTF)
2019-10-31
Alternative Title
Study on the lateral sloshing behavior under microgravity condition targeted for a propellant tank
Periodical title
International journal of microgravity science and application : IJMSA
No. or year of volume/issue
36(4)
Volume
36(4)
ISSN (Periodical Title)
2188-9783
ISSN-L (Periodical Title)
0915-3616
Text Language Code
jpn
Persistent ID (NDL)
info:ndljp/pid/11488733
Collection (Materials For Handicapped People:1)
Collection (particular)
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
Acquisition Basis
オンライン資料収集制度
Date Accepted (W3CDTF)
2020-05-14T20:27:18+09:00
Date Captured (W3CDTF)
2020-05-14
Format (IMT)
application/pdf
Access Restrictions
国立国会図書館内限定公開
Service for the Digitized Contents Transmission Service
図書館・個人送信対象外
Availability of remote photoduplication service
Periodical Title (Persistent ID (NDL))
info:ndljp/pid/11488728
Data Provider (Database)
国立国会図書館 : 国立国会図書館デジタルコレクション

Digital

Summary, etc.
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
Access Restrictions
インターネット公開
Data Provider (Database)
科学技術振興機構 : J-STAGE

Digital

Summary, etc.
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.
Access Restrictions
インターネット公開
Data Provider (Database)
国立情報学研究所 : CiNii Research
Original Data Provider (Database)
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
NAID
130007739893