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低ブーム圧力波形の実現に関する数値解析
https://jaxa.repo.nii.ac.jp/records/37141
https://jaxa.repo.nii.ac.jp/records/37141d5e3ecb5-0239-4c77-a59c-b992d74b74f0
名前 / ファイル | ライセンス | アクション |
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nalsp0037015.pdf (648.1 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 | 低ブーム圧力波形の実現に関する数値解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SST | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速輸送機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソニックブーム低減 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低ブーム圧力波形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最小2乗法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力不一致 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 近傍場圧力波形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 胴体形状最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力波形パラメータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波伝搬 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形理論 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SST | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic transport | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sonic boom reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low boom pressure signature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | least squares method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure discrepancy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | near field pressure signature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuselage geometry optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure signature parameter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave propagation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linear theory | |||||
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 for generating low-boom pressure signatures | |||||
著者 |
牧野, 好和
× 牧野, 好和× 綿貫, 忠晴× 久保田, 弘敏× 青山, 剛史× 高木, 亮治× 岩宮, 敏幸× Makino, Yoshikazu× Watanuki, Tadaharu× Kubota, Hirotoshi× Aoyama, Takashi× Takaki, Ryoji× Iwamiya, Toshiyuki |
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著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
東京大学 大学院 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo Graduate School | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 37, p. 93-98, 発行日 1998-02 |
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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 12-13 Jun. 1997 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 12-13 Jun. 1997 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 数値最適化法により、ソニックブーム減少に関する空力設計を研究した。本設計法は3次元オイラーCFD(数値流体力学)コードに最小2乗最適化法を組合わせた。目標とする低ブーム圧力波形と計算した近傍場圧力波形との圧力の不一致を最小にするため、本手法により航空機の胴体形状を修正した。研究の結果、本手法により設計した航空機形状は低ブーム圧力波形を生成し得ることを示した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A study of the aerodynamic design for the reduction of sonic-boom is conducted by a numerical optimization method. The design method combines a three-dimensional Euler CFD (Computational Fluid Dynamics) code with a least-square optimization technique. The fuselage geometry of an aircraft is modified by the method in order to minimize the pressure discrepancy between a target low-boom pressure signature and a calculated near-field pressure signature. The results of the study indicate that the aircraft configuration designed by the method can generate the low-boom pressure signature. | |||||
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: AA0001433015 | |||||
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-37 |