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有翼往還機型模型フラッタ特性へのロールモードの影響
https://jaxa.repo.nii.ac.jp/records/37395
https://jaxa.repo.nii.ac.jp/records/37395d9a5a95a-2fd7-4ec2-8e1d-dc65816a927d
名前 / ファイル | ライセンス | アクション |
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nalsp0042015.pdf (726.3 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 有翼往還機型模型フラッタ特性へのロールモードの影響 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有翼宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2ロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロール弾性モード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 曲げフラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 捩れフラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 逆対称モードフラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロール用スティング支持装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限要素法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空気力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ダブルポイント法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DPM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | winged space vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | elastic rolling mode | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bending mode flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | torsional mode flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | anti symmetric mode flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sting support for roll | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibrational analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite element method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamic force | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | double point method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DPM | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Effects of rolling mode on flutter characteristics of re-entry space vehicle model | |||||
著者 |
神田, 淳
× 神田, 淳× 上田, 哲彦× Kanda, Atsushi× Ueda, Tetsuhiko |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 42, p. 147-152, 発行日 1999-05 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 21-22 May 1998 (60th). 26-27 Nov. 1998 (61st) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 21-22 May 1998 (60th). 26-27 Nov. 1998 (61st) | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 有翼往還実験機HOPE-X(宇宙往還技術試験機)計画が、現在進行中である。この試験機をH-2ロケットに結合・搭載して打ち上げる際には、ロール弾性モードが、動力学特性の1つになろう。そこで、このような形態を模擬したフラッタ実験を遷音速風洞において行った。主翼の曲げおよび捩れフラッタが、逆対称モードで生じた。このフラッタは、ロール用弾性支持装置を用いると、ロールフリー(バネ無し)の場合より低い動圧で生じた。さらに、この種のフラッタは非定常空気力にDPM(ダブルポイント法)を用いた数値解析でも確認した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A project of experimental winged space vehicle HOPE-X (H 2 Orbiting Plane Experimental) is on going. An elastic rolling mode may be involved in the dynamic characteristics at the launching configuration of this vehicle which is attached to the H-2 rocket. Flutter experiments of a HOPE-like configuration model were made in a transonic wind tunnel. As the results, a wing bending torsional mode flutter occurred in anti-symmetric mode. It was observed that the flutter occurred in lower dynamic pressure in the case of elastic support for roll than in roll free case. Further, this type of flutter was confirmed in the numerical analysis with the unsteady aerodynamic forces by DPM (Double Point Method). | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001959015 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-42 |