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アイテム
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最適飛行経路を持つ翼胴一体型フライバックブースタ段形状の空力/空力加熱/構造重量最適設計
https://jaxa.repo.nii.ac.jp/records/2944
https://jaxa.repo.nii.ac.jp/records/294425553e8b-8695-43ee-9808-8fa7547b3c62
名前 / ファイル | ライセンス | アクション |
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AA1830029015.pdf (3.6 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | 最適飛行経路を持つ翼胴一体型フライバックブースタ段形状の空力/空力加熱/構造重量最適設計 | |||||
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_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 | Design Optimization of Blended-Wing-Body-Type Flyback Booster with Optimal Trajectory in View of Aerodynamics, Aerodynamic Heating, and Structural Weight | |||||
著者 |
住元, 剛志
× 住元, 剛志× 千葉, 一永× 金崎, 雅博× 藤川, 貴弘× 米本, 浩一× Sumimoto, Tsuyoshi× Chiba, Kazuhisa× Kanazaki, Masahiro× Fujikawa, Takahiro× Yonemoto, Koichi |
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著者所属 | ||||||
電気通信大学 | ||||||
著者所属 | ||||||
電気通信大学 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Electro-Communications | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Electro-Communications | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-18-005, p. 141-146, 発行日 2019-02-25 |
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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 | 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎 | |||||
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 | 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have implemented the design optimization of the three-dimensional geometry for a two-stage-to-orbit flyback booster under six objective functions regarding aerodynamics, aerodynamic heating, and structures to obtain the knowledge for designing reusable launch vehicle. It is important to view the relationship among the objective functions of other fields with aerodynamic heating under designing spacecraft. We defined many-objective problem to execute more realistic configuration design based on WInged REusable Sounding rocket of Kyushu Institute of Technology and feedback the design knowledge. Accordingly, we used evolutionary computation as the optimization method and applied Strength Pareto Evolutionary Algorithm 2 as evolutionary algorithm for searching design variable space and getting design information. Moreover, data analysis was carried out for the optimization result to reveal information in the design space. Consequently, we need to consider the strictly different design strategy for the speed range between the transonic and the supersonic as well as hypersonic conditions. We also revealed that the design strategy of configuration which improves each objective function. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1830029015 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-18-005 |