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D-SEND#1 形状に対する機体近傍場圧力波形推算手法検証
https://jaxa.repo.nii.ac.jp/records/4255
https://jaxa.repo.nii.ac.jp/records/4255b2ce5939-9543-4d31-9332-80eefb4ccfad
名前 / ファイル | ライセンス | アクション |
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61958015.pdf (1.7 MB)
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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 | D-SEND#1 形状に対する機体近傍場圧力波形推算手法検証 | |||||
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 | Validation of Near-field Pressure Signature Prediction Methods Using D-SEND#1 Models | |||||
著者 |
牧野, 好和
× 牧野, 好和× 野口, 正芳× 村上, 桂一× 橋本, 敦× 金森, 正史× 石川, 敬掲× 牧本, 卓也× 内田, 貴也× 大林, 茂× 今泉, 貴博× 鈴木, 角栄× 豊田, 篤× 佐宗, 章弘× Makino, Yoshikazu× Noguchi, Masayoshi× Murakami, Keiichi× Hashimoto, Atsushi× Kanamori, Masashi× Ishikawa, Hiroaki× Makimoto, Takuya× Uchida, Takaya× Obayashi, Shigeru× Imaizumi, Takahiro× Suzuki, Kakuei× Toyoda, Atsushi× Sasoh, Akihiro |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部機体システム研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部機体システム研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
三向ソフトウェア開発 | ||||||
著者所属 | ||||||
菱友システムズ | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Sankosoft Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
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 en : JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 巻 JAXA-SP-12-010, p. 89-94, 発行日 2013-03-29 |
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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44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県 | |||||
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 | 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Some numerical analysis tools for predicting near-field pressure signatures of a supersonic airplane are validated with wind tunnel test data and ballistic range test data. Two model configurations of the first phase of JAXA’s low-sonic-boom concept demonstration project(DSEND#1) are used in this study. Five kinds of numerical analysis tools, a panel analysis with aging modification, an axisymmetric Euler CFD, an unstructured grid Euler CFD, a structured/unstructured overset grids Euler CFD, and a hexagrid Euler CFD, are applied to these models for predicting their near-field pressure signatures at Mach number of 1.4 and 1.7. The predicted signatures are compared with the supersonic wind tunnel data of the 5% models and the ballistic range data of the 1.6% models. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 著者人数: 13名 | |||||
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 | Number of authors: 13 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061958015 | |||||
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-12-010 |