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逆解法を用いた翼胴一体化設計について
https://jaxa.repo.nii.ac.jp/records/43451
https://jaxa.repo.nii.ac.jp/records/43451c02f9bb4-512d-4bea-9327-5ef7f5a7ac42
名前 / ファイル | ライセンス | アクション |
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nalsp0014018.pdf (1.2 MB)
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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 | 逆解法を用いた翼胴一体化設計について | |||||
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 | Blended Wing-Body Configuration Design using Transonic Inverse Code | |||||
著者 |
谷, 泰寛
× 谷, 泰寛× 越岡, 康弘× 廣瀬, 秀大× Tani, Yosuhiro× Koshioka, Yasuhiro× Hirose, Hidehiro |
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著者所属 | ||||||
富士重工業株式会社 | ||||||
著者所属 | ||||||
富士重工業株式会社 | ||||||
著者所属 | ||||||
富士重工業株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
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-14 巻 14, p. 115-120, 発行日 1990-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, using a three dimensional transonic inverse method with target pressure distribution. In this application, it is combined with a full potential analysis code. Some of the design results for a conventional and a blended wing-body configuration are presented. Also a finite volume Euler solver is applied to analyze the designed configurations. | |||||
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: NALSP0014018 | |||||
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-14 |