{"created":"2023-06-20T14:36:16.944068+00:00","id":2597,"links":{},"metadata":{"_buckets":{"deposit":"797ecdef-0c2e-4a80-9691-4e7294a146fb"},"_deposit":{"created_by":1,"id":"2597","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2597"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002597","sets":["1887:1893","9:1090:1241:1251"]},"author_link":["7614","7620","7616","7617","7619","7611","7624","7612","7621","7622","7623","7615","7618","7613"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Euler/LEE code for acoustic load evaluation during rocket launch: Second volume. LEE option"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-02-27","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RM-08-009","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":"ロケット打ち上げ時に生じる構造振動や内部騒音の主因となる音響荷重を予測することは重要である。この予測は、従来、経験的手法によって行われてきたが、そうした手法では音響伝播過程における遮蔽や反射が考慮されていない。こうした問題を解決するために、我々はEuler/LEEコードを開発し、H-IIAの打ち上げ射場の音響評価に応用してきた。本報告では、第1報に引き続き当コードのLEEオプションの使用方法を解説する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Acoustic loads are the principal source of structural vibration and internal noise during launch. Therefore, it is important to predict the acoustic loads on spacecraft such as a rocket. Conventionally, the prediction has been made by empirical methods. In these methods shielding and reflection are not considered. To solve these problems, we have been developing an Euler/LEE(Linearized Euler Equation) hybrid code and applying it to the acoustic evaluation of H-IIA's launch pad. In this report, we explain how to use the LEE option of the hybrid code.","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_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064260000","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-08-009","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":"計算力学研究センター"},{"subitem_text_value":"計算力学研究センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部数値解析センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部数値解析センター"},{"subitem_text_value":"宇宙航空研究開発機構情報・計算高額センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部数値解析センター"},{"subitem_text_value":"名古屋大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Research Center of Computational Mechanics Inc."},{"subitem_text_language":"en","subitem_text_value":"Research Center of Computational Mechanics Inc."},{"subitem_text_language":"en","subitem_text_value":"Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"JAXA's Engineering Degital Innovation Center, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岩永, 則城"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"金田, 英和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村上, 桂一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 敦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"北村, 圭一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青山, 剛史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 佳朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwanaga, Noriki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaneda, Hidekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murakami, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kitamura, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoyama, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiaki","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":"64260000.pdf","filesize":[{"value":"7.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64260000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2597/files/64260000.pdf"},"version_id":"caeed78e-a929-48b4-ae19-027c081b4a80"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Euler/LEE code, Acoustic loads, Rocket","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":"ロケット打ち上げ時の音響環境を評価するEuler/LEEコード: 第2報. LEEオプション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケット打ち上げ時の音響環境を評価するEuler/LEEコード: 第2報. LEEオプション"}]},"item_type_id":"3","owner":"1","path":["1251","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2597","relation_version_is_last":true,"title":["ロケット打ち上げ時の音響環境を評価するEuler/LEEコード: 第2報. LEEオプション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:19:22.705509+00:00"}