境界要素法による全機形態の非定常空力計算

Material type: 文書・図像類

Author: 柳沢, 三憲ほか

Publisher: 航空宇宙技術研究所

Publication date: 1987-11

Material Format: Digital

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Note (General)：: A boundary element method is presented for determining aerodynamic loadings on arbitrary configurations in oscillatory subsonic flow. Formulas (modifi...

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Material Type: 文書・図像類
Title: 境界要素法による全機形態の非定常空力計算
Author/Editor: 柳沢, 三憲
森田, 甫之
巽, 重文
Yanagizawa, Mitsunori
Morita, Toshiyuki
Tatsumi, Shigefumi
Author Heading: 柳沢, 三憲
森田, 甫之
巽, 重文
Yanagizawa, Mitsunori
Morita, Toshiyuki
Tatsumi, Shigefumi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1987-11
Publication Date (W3CDTF): 1987-11
Alternative Title: Calculations of Unsteady Aerodynamics for a Full Aircraft Configuration Using Boundary Element Method
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-8
No. or year of volume/issue: 8
Volume: 8
Pages: 91-102
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): A boundary element method is presented for determining aerodynamic loadings on arbitrary configurations in oscillatory subsonic flow. Formulas (modified Morino's method) are given for the unsteady pressure distributions or unsteady force experienced in subsonic flow by the wing-store combination, oscillating in the torsional oscillations about a fixed axis parallel to the span and other oscillating modes (flapping, plunging). Interference effects from an underwing pylon store were analyzed. The method is finally verified through comparison with experiment for the model at angles of attack from -5 degree to +5 degree, and reduced frequencies from 0.65 to l.3 at low subsonic flow.
資料番号: NALSP0008013
レポート番号: NAL SP-8
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
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