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遷音速域における振動翼まわりの数値解析
https://jaxa.repo.nii.ac.jp/records/36789
https://jaxa.repo.nii.ac.jp/records/3678942ec9627-69b5-455d-ba91-a24150f8f520
名前 / ファイル | ライセンス | アクション |
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nalsp0030021.pdf (2.2 MB)
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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 | ||||||
タイトル | 遷音速域における振動翼まわりの数値解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動翼周りの流れ | |||||
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Navier-Stokes方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力弾性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Beam-Warming ADI法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 薄翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スレンダ翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 格子形成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非粘性流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 差分法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常空気力学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow around oscillating wing | |||||
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 Navier Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aeroelasticity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Beam Warming ADI method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thin wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | slender wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | grid generation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numeral analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inviscid flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite difference method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady aerodynamics | |||||
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(英) | ||||||
その他のタイトル | Numerical simulation of the flowfield around an oscillating wing in transonic range | |||||
著者 |
石黒, 満津夫
× 石黒, 満津夫× 巽, 重文× 中道, 二郎× Ishiguro, Mitsuo× Tatsumi, Shigefumi× Nakamichi, Jiro |
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著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries, Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 30, p. 115-120, 発行日 1996-01 |
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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 7-9 Jun. 1995 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 7-9 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 空力弾性の分野では、従来、空力弾性の予測には非粘性の非定常空気力学が用いられてきた。最近ではスーパーコンピュータの進歩を考慮し、振動翼周りの非定常流れ場のNavier-Stokes方程式ベースの数値シミュレーションが一般的になった。振動翼周りの非定常Navier-Stokes方程式を解く計算機コードを開発した。本コードはBeam-Warming ADI法をベースとし、ダイナミック格子形成システムと連結する。ここでは薄翼で低アスペクト比の振動翼に本コードを適用する場合の統合定式化について述べた。コンピュータの計算結果はNALの2m遷音速風洞での試験データと比較検討した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the field of aeroelasticity, inviscid unsteady aerodynamics have traditionally been used to predict aeroelastic phenomena. However, thanks to the recent advance of supercomputer, numerical simulation of unsteady flowfield around an oscillating wing based on the Navier-Stokes equations has become popular. Recently a computer code which is capable of solving unsteady Navier-Stokes equations around oscillating wings was developed. The code is based on the Beam-Warming ADI (Alternating Direction Implicit) method combined with a dynamic grid system. This paper describes the formulation of the method together with the application of the code to an oscillating wing which has the low aspect ratio and low thickness ratio. The correlation work of the computer results with the wind tunnel test data which are obtained at NAL 2 m transonic wind tunnel is also presented. | |||||
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: AA0000294021 | |||||
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-30 |