{"created":"2023-06-20T14:54:09.376954+00:00","id":22422,"links":{},"metadata":{"_buckets":{"deposit":"dd29fac6-7c56-4f5d-9037-d9b66aff4cfa"},"_deposit":{"created_by":1,"id":"22422","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22422"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022422","sets":["1887:1888"]},"author_link":["210242","210246","210244","210241","210245","210240","210247","210243"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Theory Review and Test Verification about Combination of FEA and SEA Methods to Predict the Vibroacoustic Response of Spacecraft Structure"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-06","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"802","bibliographicPageEnd":"1969","bibliographicPageStart":"1960","bibliographicVolumeNumber":"79","bibliographic_titles":[{"bibliographic_title":"日本機械学會論文集 C編"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Spacecraft is exposed to the severe random vibration by acoustic during its launch. In the spacecraft design, random vibration of spacecraft components mounted on panel structure during launch environments needs to be predicted. In the present methods, SEA is the method for analyzing the high frequency band, FEA is for the low frequency band. This paper applies combination of FEA and SEA methods to predict the vibroacoustic response of spacecraft structure which may be extended to wide frequency range experienced during the launch. The combination methods focuses on the vibroacoustic prediction which keeps advantages to use detail model of structure expressed by FEA and statistical energy approach expressed by SEA of reverberant acoustic excitation. The combination method is applied to diffuse sound field excitation of honeycomb panel, and is compared with acoustic excitation test and the results from conventional approach of BEM ,joint acceptance and SEA.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1410058000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本機械学会"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.1299/kikaic.79.1960"}],"subitem_relation_type":"isVersionOf","subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.1299/kikaic.79.1960","subitem_relation_type_select":"DOI"}}]},"item_7_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"（C）2013 日本機械学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0387-5024","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00187463","subitem_source_identifier_type":"NCID"}]},"item_7_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)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_7_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)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency(JAXA)"}]},"item_7_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"赤城, 弘樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 成将"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳瀬, 恵一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"施勤, 忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Akagi, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Shigemasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagase, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shi, Qinzhong","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":"2020-01-22"}],"displaytype":"detail","filename":"PA1410058.pdf","filesize":[{"value":"829.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"PA1410058.pdf","url":"https://jaxa.repo.nii.ac.jp/record/22422/files/PA1410058.pdf"},"version_id":"64beecd7-4712-422d-acec-757182471738"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Acoustic; Statistical Energy Analysis; Random Vibration; Space Engineering; Joint Acceptance; FEA; Diffuse Sound Field","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"宇宙機音響振動応答予測に関するFEA-SEA統合法適用の理論検討と実験検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"宇宙機音響振動応答予測に関するFEA-SEA統合法適用の理論検討と実験検証"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22422","relation_version_is_last":true,"title":["宇宙機音響振動応答予測に関するFEA-SEA統合法適用の理論検討と実験検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:21:26.450252+00:00"}