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ソニックブーム推算手法検証風洞試験における主翼空力弾性変形効果
https://jaxa.repo.nii.ac.jp/records/3238
https://jaxa.repo.nii.ac.jp/records/323899cf8de8-759e-4841-9fd3-e3d37bd14b69
名前 / ファイル | ライセンス | アクション |
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AA1730011004.pdf (3.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-12-28 | |||||
タイトル | ||||||
タイトル | ソニックブーム推算手法検証風洞試験における主翼空力弾性変形効果 | |||||
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 | Aeroelastic Deformation Effects of the Main Wing in the Wind-tunnel Test for Validating Sonic-boom Prediction Methods | |||||
著者 |
近藤, 賢
× 近藤, 賢× 上野, 篤史× 平野, 義鎮× 野口, 正芳× 牧野, 好和× 石川, 敬掲× Kondo, Satoshi× Ueno, Atsushi× Hirano, Yoshiyasu× Noguchi, Masayoshi× Makino, Yoshikazu× Ishikawa, Hiroaki |
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著者所属 | ||||||
株式会社菱友システムズ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
株式会社エイ・エス・アイ総研 | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Science & Intelligence Research Institute (ASIRI) | ||||||
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49回流体力学講演会/第35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 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-17-004, p. 39-45, 発行日 2017-12-27 |
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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49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-34日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京 | |||||
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 | 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The demand of Supersonic Transport (SST) is increasing globally. Some companies have announced their program for developing civil supersonic airplanes and the International Civil Aviation Organization (ICAO) has started developing the sonic boom standard for supersonic overland flight. Second AIAA Sonic Boom Prediction Workshop (SBPW2) has been held in January 2017 to assess the state of the art for predicting sonic boom. Japan Aerospace Exploration Agency (JAXA) designed a simple low boom configuration named 'JAXA Wing Body (JWB)' and provided it to the workshop for one of the test cases of SBPW2. For the validation of sonic boom prediction method, the supersonic wind-tunnel test of the JWB model was carried out at JAXA's supersonic wind-tunnel. This paper reports the development of an aeroelastic deforming estimation tool of the main wing in wind tunnel test and the results of CFD analysis for prediction of near-field sonic boom signature with aeroelastic deformation effects. | |||||
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: AA1730011004 | |||||
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-17-004 |