Study on Vibration Suppression System Using Thin Film with Viscous Lamina
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- Okubo Hiroshi
- 日産自動車(株)3-3-3推進部
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- Watanabe Naoyuki
- 東京都立科学技術大学航空宇宙システム工学科
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- Minesugi Kenji
- 宇宙航空研究開発機構宇宙科学研究本部
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- Onoda Junjiro
- 宇宙航空研究開発機構宇宙科学研究本部
Bibliographic Information
- Other Title
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- 粘着層付き薄膜を有する制振機構に関する研究
- ネンチャクソウ ツキ ハクマク オ ユウスル セイシン キコウ ニ カンスル ケンキュウ
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Abstract
Passive damping augmentation is one of attractive methods for vibration suppression to various kinds of structures because it is definitely stable and generally simple. The system using thin film with viscous adhesive indicated a remarkable effect to the vibration suppression in the practical application to a satellite. To investigate its damping characteristic, several kinds of experiments have been performed. The results show that the non-linear behavior cause of non-Newtonian flow between shear load and shear deformation velocity in the viscous lamina of the thin film contributes to the damping capability. A mathematical model which consists of spring elements as film and friction elements as viscous lamina has been proposed from experiments. The simulational results with this present model are in good agreement with experimental ones.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 53 (613), 43-50, 2005
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679447547136
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- NII Article ID
- 10014357741
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 7255568
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed