書誌事項
- タイトル別名
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- Cable Flutter Analysis of ALFLEX.
- コガタ ジドウ チャクリク ジッケン ノ ケーブルフラッタ カイセキ
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This paper introduces the flutter phenomenon occurring in the automatic landing flight experiment for a Japanese unmanned space shuttle of HOPE-X. The experimental vehicle called ALFLEX which was a dynamically scaled model of HOPE-X was towed by one cable before its release. An oscillation was observed on the cable with release device during flights of towing configuration in the preliminary tests. The analysis revealed that the oscillation was caused by the coupling between unsteady aerodynamic forces of the release device and restoring forces of the cable. The flutter could be eliminated by mass balancing before the automatic landing flight.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 46 (537), 581-583, 1998
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282679455872000
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- NII論文ID
- 10002863183
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 4575710
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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
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可