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オイラー方程式による翼ナセル干渉解析
https://jaxa.repo.nii.ac.jp/records/43221
https://jaxa.repo.nii.ac.jp/records/432212c578b87-db2b-4049-bee1-c62cdf432b4c
名前 / ファイル | ライセンス | アクション |
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nalsp0007005.pdf (446.6 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | オイラー方程式による翼ナセル干渉解析 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A Numerical Investigation on Wing/Nacelle Interferences | |||||
著者 |
沢田, 恵介
× 沢田, 恵介× 高梨, 進× Sawada, Keisuke× Takanashi, Susumu |
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著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Co. 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 SP-7 巻 7, p. 39-44, 発行日 1986-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A numerical investigation of wing/nacelle interferences of USB configuration was carried out. A grid system about the realistic configuration of wing/nacelle combination was generated by the multi-block grid generation technique. The Euler equations were solved by the second order accurate upwind scheme. Results were obtained for M infinity = 0.7, alpha = 2.0. The existence of channel flows accompanied by strong shocks between two engine nacelles were confirmed. Power effects of two engines were examined by modeling both the plane of intake and that of jet exhaust appropriately. | |||||
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: NALSP0007005 | |||||
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-7 |