| 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 |
An Experimental Investigation on Transonic Flutter Characteristics of Low Aspect-Ratio Sweptback All-Moving Horizontal Tail Surface Modesl |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 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 |
|
|
その他のタイトル |
低アスペクト比後退角付の全可動水平尾翼の遷音速フラッタ特性に関する実験的研究 |
| 著者 |
中井, 暎一
森田, 甫之
菊池, 孝男
NAKAI, Eiichi
MORITA, Toshiyuki
KIKUCHI, Takao
|
| 著者所属 |
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航空宇宙技術研究所機体第二部 |
| 著者所属 |
|
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航空宇宙技術研究所機体第一部 |
| 著者所属 |
|
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航空宇宙技術研究所機体第一部 |
| 著者所属（英） |
|
|
|
en |
|
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Second Airframe Division, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
|
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|
en |
|
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First Airframe Division, National Aerospace Laboratory(NAL) |
| 著者所属（英） |
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|
en |
|
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First Airframe Division, National Aerospace Laboratory(NAL) |
| 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 TR-643
巻 643,
p. 14,
発行日 1981-02
|
| 抄録（英） |
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|
内容記述タイプ |
Other |
|
内容記述 |
An experimental investigation has been conducted on the transonic flutter characteristics of low aspect ratio thin sweptback all-moving tail surface models, which were supported by a simulated fuselage beam. These experiments were conducted in the NAL 60cm×60cm transonic blowdown wind tunnel for flutter testing, at Mach numbers from 0.873 to 1.129. The tail surface has sweptback angles of 42.5deg at the leading edge and 10deg at the trailing edge, an aspect ratio of 1.394, and a taper ratio of 0.318. The wing models have been supported by the narrow width at the root. Some effects of an added mass at the leading edge of the wing tip on the flutter characteristics were also studied. Added mass improved the transonic flutter characteristics. It is concluded that the flutter boundaries for the tail surface models were obtained, and that the flutter boundaries expressed by the experimental flutter speed coefficients are characterized by having a minimum value at around Mach number 1.0 in the range of Mach numbers used. |
| ISSN |
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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: NALTR0643000 |
| 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-643 |
naltr00643.pdf (798.0 kB)
