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Numerical simulation of viscous unsteady flow around wing oscillating in elastic modes
https://jaxa.repo.nii.ac.jp/records/36909
https://jaxa.repo.nii.ac.jp/records/3690967d8f2cf-0491-428a-9be8-fa2a059f53d8
名前 / ファイル | ライセンス | アクション |
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nalsp0034050.pdf (453.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Numerical simulation of viscous unsteady flow around wing oscillating in elastic modes | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 弾性モード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常粘性流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常遷音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高アスペクト比 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動弾性翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速フラッタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | elastic mode | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | viscous unsteady flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady transonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high aspect ratio | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structural equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oscillating elastic wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation | |||||
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 | ||||||
その他のタイトル | 弾性モードで振動する翼周りの非定常粘性流の数値シミュレーション | |||||
著者 |
Kheirandish, Hamidreza
× Kheirandish, Hamidreza× 別府, 護朗× 中道, 二郎× Kheirandish, Hamidreza× Beppu, Goro× Nakamichi, Jiro |
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著者所属 | ||||||
東海大学 工学部 航空宇宙学科 | ||||||
著者所属 | ||||||
東海大学 工学部 航空宇宙学科 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 構造力学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University Department of Aeronautics and Astronautics, School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University Department of Aeronautics and Astronautics, School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Structural Mechanics 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特別資料 en : Special Publication of National Aerospace Laboratory 巻 34, p. 285-288, 発行日 1997-01 |
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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 | 航空宇宙技術研究所 6-7 JUN. 1996 東京 日本 | |||||
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 | National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 空力弾性型CFD(数値流体力学)コードを開発し、曲げモードで振動するバイオコンベックス翼断面を持つ矩形翼、および第一曲げモードで振動する高アスペクト比(YXX)翼の風洞モデルまわりの非定常遷音速流れの数値シミュレーションに適用した。第一の6つのモードを考慮してYXX翼の遷音速フラッタについても同様に数値シミュレーションを実施した。構造方程式と組合わせたナビエ・ストークス(N-S)方程式に基づくコードを用いた。N-S方程式は空力格子上のYee-Harten TVD(Total Variation Diminishing)スキームを用いて積分し、構造方程式はWilsonθ法を用いて積分した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An aeroelastic version of CFD (Computational Fluid Dynamics) code was developed and applied to numerical simulations of unsteady transonic flows around a rectangular wing with bioconvex airfoil section oscillating in bending mode and a wing tunnel model of a high aspect-ratio (YXX) wing which is also oscillating in first bending mode. A numerical simulation of transonic flutter of the YXX wing considering first six modes has been performed as well. The code is based on Navier-Stokes (N-S) equations coupled with the structural equations. The N-S equations are integrated by Yee-Harten TVD (Total Variation Diminishing) scheme on dynamic grid, while the structural side is integrated by Wilson theta 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: AA0000685050 | |||||
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-34 |