{"created":"2023-06-20T14:37:05.861195+00:00","id":3482,"links":{},"metadata":{"_buckets":{"deposit":"860b3247-8af5-483d-9b8d-4bc15e3eb62f"},"_deposit":{"created_by":1,"id":"3482","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3482"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003482","sets":["1398:1530:1533","1543:1874:1877","1887:1891","9:789:817:1980"]},"author_link":["13828","13829","13831","13833","13830","13832"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aft-Boom Shaping for Small Supersonic Transport and Validation by Wind Tunnel Test"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-12-27","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"79","bibliographicVolumeNumber":"JAXA-SP-16-007","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第48回流体力学講演会/第34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"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aft-boom shaping for a small supersonic transport is performed and is validated by the wind tunnel test. First, the parametric study of horizontal stabilizer shape using the low-fidelity design tool is conducted in order to fragment the aft boom into two shock waves. Though the nacelle is not modeled in this design, the negative effect of nacelle pressure waves on the aft-boom is considered, and pressure waves caused by the horizontal stabilizer is strengthened to realize the fragmentation. Results show the importance of inverse camber and extended root chord length in order to realize both low-drag and low-boom. Then, wind tunnel test and high-fidelity CFD (FaSTAR) analysis for the designed shape without nacelle are performed. Near-field pressure signatures obtained by wind tunnel test and FaSTAR analysis agree well. Finally, FaSTAR analysis is performed for the designed shape with nacelle and shows that the aft-boom is successfully fragmented into two shock waves even though the coalescence of these two shock waves is advanced by the nacelle expansion wave.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630031007","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-16-007","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"上野, 篤史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"牧野, 好和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Yoshikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"AA1630031007.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630031007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3482/files/AA1630031007.pdf"},"version_id":"c5611cd5-f13e-43c9-b3dd-48b095a9fd00"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"小型超音速旅客機の後端低ブーム設計と風洞試験による検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型超音速旅客機の後端低ブーム設計と風洞試験による検証"}]},"item_type_id":"5","owner":"1","path":["1533","1877","1891","1980"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-01-13"},"publish_date":"2017-01-13","publish_status":"0","recid":"3482","relation_version_is_last":true,"title":["小型超音速旅客機の後端低ブーム設計と風洞試験による検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:01:13.142861+00:00"}