{"created":"2023-06-20T15:10:43.399700+00:00","id":40298,"links":{},"metadata":{"_buckets":{"deposit":"285473fb-5662-45ab-ba44-a310f157219a"},"_deposit":{"created_by":1,"id":"40298","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40298"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040298","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["447167","447165","447164","447166"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Ground vibration tests of an aging aircraft"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"11","bibliographicPageStart":"1","bibliographicVolumeNumber":"732","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"動的変位計測装置を用いて経年機(FA-200-180型)の全機地上振動試験を行った。機体は、航空大学校で約12,000時間の飛行訓練に使用されたものである。試験は、2点相関ランダム加振による伝達関数法を用いた。その結果、対称と逆対称モードの分離を行うことができ、主翼の固有振動数とノーダルラインは開発時に行われた試験結果とほぼ等しく、両者の間に振動特性の顕著な相違は認められなかった。また、動的変位計測装置が実機の振動試験に有効な装置であることを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Full scale ground vibration tests were carried out on an aged FA-200-180 aircraft by using a dynamic displacement measurement system. The test aircraft has been used in training for about 12,000 hours at the Civil Aviation College. The transfer function method with dual correlated random excitation was adopted in this test. The test results showed that several vibration modes were separated and that the resulting natural frequencies and nodal lines were similar to those of the original prototype aircraft. The vibration characteristics did not show any appreciable difference between the aged aircraft and the original prototype aircraft. It is also confirmed that the dynamic displacement measurement system operated effectively for full scale vibration tests.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001658000","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: NAL TM-732","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"外崎, 得雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 哲彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sotozaki, Tokuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Tetsuhiko","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm0000732.pdf","filesize":[{"value":"476.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000732.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40298/files/naltm0000732.pdf"},"version_id":"ce492964-b7f8-4bf9-8f38-46b1308fd3c7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"経年航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"地上振動試験","subitem_subject_scheme":"Other"},{"subitem_subject":"プロペラ機","subitem_subject_scheme":"Other"},{"subitem_subject":"固有振動モード","subitem_subject_scheme":"Other"},{"subitem_subject":"主翼ノーダルライン","subitem_subject_scheme":"Other"},{"subitem_subject":"振動試験システム","subitem_subject_scheme":"Other"},{"subitem_subject":"FA-200-180","subitem_subject_scheme":"Other"},{"subitem_subject":"変位計測ロボット","subitem_subject_scheme":"Other"},{"subitem_subject":"2点相関ランダム加振","subitem_subject_scheme":"Other"},{"subitem_subject":"aged aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground vibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propeller aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"natural vibration mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"main wing nodal line","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FA 200 180","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"displacement measuring robot","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dual correlated random excitation","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":"経年航空機の全機地上振動試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"経年航空機の全機地上振動試験"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40298","relation_version_is_last":true,"title":["経年航空機の全機地上振動試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:16:10.413465+00:00"}