{"created":"2023-06-20T14:36:16.266991+00:00","id":2582,"links":{},"metadata":{"_buckets":{"deposit":"525e97bf-67e8-484b-82c1-bcb0762910b1"},"_deposit":{"created_by":1,"id":"2582","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2582"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002582","sets":["1887:1893","9:1090:1230:1235"]},"author_link":["7487","7485","7488","7486"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Preliminary Supersonic Wind Tunnel Test for Low Sonic-boom Design Validation of Silent Supersonic Technology Demonstrator"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-01-29","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RM-09-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"低ソニックブーム設計技術の実証を第一の目的とする静粛超音速研究機の基本設計において，低ブーム設計検証のためにJAXA1m×1m超音速風洞において機体近傍場の圧力分布計測を実施した．計測された圧力波形は設計時の数値解析結果と同様に，低ブーム特性を示していることが確認された．また，マッハ数や迎角，ロール角等の飛行条件がブーム特性に与える影響について調べ，研究機に求められる飛行制御要求の妥当性についても検証した．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Near-field pressure signatures of the silent supersonic technology demonstrator are measured in the JAXA 1 m x 1 m supersonic wind tunnel in its preliminary design phase for validating its low sonic-boom design. The low sonic-boom features are observed in the measured pressure signatures which are compared to those predicted by some CFD codes. Some flight requirements which are imposed on the demonstrator such as the retention of flight Mach number, variations in the pitch or roll angle, are validated by the comparison of near-field pressure signatures for these effects.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064576000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-09-006","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム"},{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"牧野, 好和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Yoshikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","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":"64576000.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64576000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2582/files/64576000.pdf"},"version_id":"3eac487f-629c-43fd-87c7-84836f667228"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"supersonic transport, sonic-boom, wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"静粛超音速研究機基本設計低ブーム確認超音速風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"静粛超音速研究機基本設計低ブーム確認超音速風洞試験"}]},"item_type_id":"3","owner":"1","path":["1235","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2582","relation_version_is_last":true,"title":["静粛超音速研究機基本設計低ブーム確認超音速風洞試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:19:39.272654+00:00"}