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チップフィン形状翼フラッタ低速基礎風洞実験
https://jaxa.repo.nii.ac.jp/records/41212
https://jaxa.repo.nii.ac.jp/records/41212d33d1552-8586-4154-ab1b-606cb616d5b5
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr01228.pdf (2.5 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | チップフィン形状翼フラッタ低速基礎風洞実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速フラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ解析データ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ試験モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ模型振動試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スペースプレーン形態 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | チップフィン形状 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的変位計測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マスバランス効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞内フラッタ緊急停止装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 曲げ捩り連成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 主翼方向舵連成フラッタ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter characteristics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter analysis data | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter test model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter model vibration test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spaceplane configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tip fin configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic displacement measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | mass balance effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel flutter suppression device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bending torsion coupling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing rudder coupling flutter | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Fundamental wind tunnel experiments on low-speed flutter of a tip-fin configuration wing | |||||
著者 |
上田, 哲彦
× 上田, 哲彦× 外崎, 得雄× 岩崎, 和夫× Ueda, Tetsuhiko× Sotozaki, Tokuo× Iwasaki, Kazuo |
|||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
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報告 en : Technical Report of National Aerospace Laboratory 巻 1228, p. 1-20, 発行日 1994-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | チップフィン形状翼のフラッタ特性を把握するために基礎的な風洞実験を行った。模型を2体作り非平面翼のフラッタ解析のための実験データを得た。1体は通常の平面翼であり、もう1体は15度のキャントをもってチップフィン形状翼を構成している。チップフィン形状翼において、典型的な曲げと捩りのフラッタを起こす速度より低にある速度領域でマイルドなフラッタが観測された。それは、主翼の捩り変形モードとチップフィン上にあるマスバランスのついたラダーの回転自由度が構成したものであった。動翼のマスバランスのフラッタに対する効果の検討も行った。模型の振動試験は動的変位計測装置を使って自動的に行われた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Wind tunnel tests were conducted to investigate the fundamental flutter characteristics of a tip-fin configuration wing. Two types of models were tested to provide experimental data for the flutter analysis of non-coplanar wings. One is a normally plain wing and the other has a cant angle of 15 deg at the tip-fin. They were tested in the 2 m x 2 m low-speed wind tunnel. On the tip-fin wing, mild flutter with limited amplitudes was observed in a certain range of speeds well below the typical violent flutter speed. It was caused by the coupling between wing torsions. and the deflection of the rotationally free rudder with mass balance. The effects of mass balance of the rudder located at the tip-fin were also studied to confirm its role in flutter prevention. Modal tests on the models were performed automatically using the Dynamic Displacement Measurement System. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0004242000 | |||||
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 TR-1228 |