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Prediction method of boundary layer transition in 3-D compressible flow
https://jaxa.repo.nii.ac.jp/records/36826
https://jaxa.repo.nii.ac.jp/records/36826897824cb-638b-4b03-8989-f35540570b95
名前 / ファイル | ライセンス | アクション |
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nalsp0031003.pdf (768.8 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 | Prediction method of boundary layer transition in 3-D compressible flow | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元圧縮流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層遷移 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷移位置予測法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値計算法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | N因子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算時間 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional compressible flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer transition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transition location prediction method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | calculation algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical calculation method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | N factor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | calculation time | |||||
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 | 3次元圧縮流における境界層遷移の予測法 | |||||
著者 |
石田, 洋治
× 石田, 洋治× Ishida, Yoji |
|||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics 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 31, p. 39-51, 発行日 1996-05 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 超音速翼上の境界層の遷移位置を予測するための効率的な数値計算法を提案した。この計算システムは3次元境界層、その線形安定性およびN因子の計算から構成されている。3種類の計算の各々は大量の計算時間と各計算間の複雑な干渉手続きを必要とする。従って、計算時間を節約し計算システムをできるだけ簡素なものにするために、境界層の計算と線形安定性の計算に対して同じ計算アルゴリズムを用いた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An efficient numerical calculation method for predicting the transition location of the boundary layer over a supersonic wing was proposed. This numerical system consists of the calculations of Three Dimensional (3-D) boundary layer, its linear stability characteristics, and N factor. Each of the three calculations requires a lot of computing time and a rather complex interference procedure between each calculation. Therefore, the same computing algorithm for both boundary layer and linear stability calculations was used to save computing time and to make the calculation system as simple as possible. | |||||
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: AA0000440003 | |||||
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-31 |