複合材平板を芯材にした後退翼フラッタ模型の遷音速フラッタ試験(空力弾性テーラリング効果の検討)

Material type: 文書・図像類

Author: 磯貝, 紘二ほか

Publisher: 航空宇宙技術研究所

Publication date: 1984-08

Material Format: Digital

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Note (General)：: The Effects of the fiber orientation on the transonic flutter characteristics of a sweptback wing with a core composite plate are examined experimenta...

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Material Type: 文書・図像類
Title: 複合材平板を芯材にした後退翼フラッタ模型の遷音速フラッタ試験(空力弾性テーラリング効果の検討)
Author/Editor: 磯貝, 紘二
江尻, 宏
菊池, 孝男
中道, 二郎
野口, 義男
森田, 甫之
ISOGAI, Koji
EJIRI, Hiroshi
KIKUCHI, Takao
NAKAMICHI, Jiro
NOGUCHI, Yoshio
MORITA, Toshiyuki
Author Heading: 磯貝, 紘二
江尻, 宏
菊池, 孝男
中道, 二郎
野口, 義男
森田, 甫之
ISOGAI, Koji
EJIRI, Hiroshi
KIKUCHI, Takao
NAKAMICHI, Jiro
NOGUCHI, Yoshio
MORITA, Toshiyuki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1984-08
Publication Date (W3CDTF): 1984-08
Alternative Title: Experimental Study on Transonic Flutter Characteristics of Sweptback Wing with Core Composite Plates Having Different Fiber Orientations
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-827
No. or year of volume/issue: 827
Volume: 827
Pages: 11-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): The Effects of the fiber orientation on the transonic flutter characteristics of a sweptback wing with a core composite plate are examined experimentally. For this purpose, the two kinds of flutter model having the same planform but different bend-twist characteristics were made ; one has a wash-out tendency and the other a wash-in tendency. The wing has an aspect ratio of 5.0, a taper ratio of 0.50 and a leading edge sweep angle of 45 degrees. The airfoil section of this wing is a symmetrical NACA64A010. The flutter models were tested in the National Aerospace Laboratory’s 0.6m×0.6m blowdown wind tunnel. The flutter boundaries of both the wash-in and wash-out models were determined for a wide range of the transonic Mach numbers, namely, M∞=0.80～1.20. This experiment revealed that the wash-in model shows 25～30 percent higher flutter velocities than those of the wash-out model over the entire Mach number range tested.
資料番号: NALTR0827000
レポート番号: NAL TR-827
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45085&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45085&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ