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超音速層流境界層における非粘性型不安定性
https://jaxa.repo.nii.ac.jp/records/36946
https://jaxa.repo.nii.ac.jp/records/3694649c9c6ba-74a6-4f87-afd1-180817bd3607
名前 / ファイル | ライセンス | アクション |
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nalsp0033015.pdf (451.2 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 | ||||||
タイトル | 超音速層流境界層における非粘性型不安定性 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Tollmien-Schlichting波 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形安定性理論 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVDスキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 全変動減少 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 変曲点不安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮コーナ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 膨張コーナ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 直接数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形安定性解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速境界層 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Tollmien Schlichting wave | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear stability theory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TVD scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total variation diminishing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inflectional instability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compression corner | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | expansion corner | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | direct numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear stability analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic boundary layer | |||||
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 | Inviscid instability in supersonic laminar boundary layer | |||||
著者 |
坂上, 昇史
× 坂上, 昇史× 西岡, 通男× Sakaue, Shoji× Nishioka, Michio |
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著者所属 | ||||||
大阪府立大学 工学部 | ||||||
著者所属 | ||||||
大阪府立大学 工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University College of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University College of Engineering | ||||||
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 33, p. 63-68, 発行日 1996-09 |
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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 | 28-29 Sep. 1995 (17th). 28-29 Mar. 1996 (18th) | |||||
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 | 28-29 Sep. 1995 (17th). 28-29 Mar. 1996 (18th) | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 圧縮または膨張コーナにより乱された超音速平板境界層流の不安定性を、線形安定性理論と直接数値シミュレーション(DNS)により研究した。その結果、平行流安定性理論はTollmien-Schlichting波挙動のDNS結果をよく予測できることが分かった。さらに、非粘性線形安定性解析を行ってきて、しばしば引用されるM(sub 1)=4.0より低いマッハ数2.2の領域でも、変曲点不安定性が境界層不安定性を支配することを明らかにした。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The instability of supersonic flat-plate boundary layer flow disturbed by compression or expansion corner is investigated on the basis of the linear stability theory and through Direct Numerical Simulations (DNS). It is found that the parallel-flow stability theory can well predict the DNS results for the behavior of Tollmien-Schlichting waves. Furthermore, the inviscid linear stability analysis has been made to clarify that the inflectional instability really governs the boundary layer instability at such Mach number as 2.2, being far below the often cited value M(sub 1) = 4.0. | |||||
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: AA0000867015 | |||||
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-33 |