{"created":"2023-06-20T15:15:16.865009+00:00","id":45354,"links":{},"metadata":{"_buckets":{"deposit":"075ddeab-b425-4ab3-9b9d-40c01efabfe8"},"_deposit":{"created_by":1,"id":"45354","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45354"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045354","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474319","474317","474320","474318"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Theoretical Estimation of the Viscous Damping from Liquid Transient Motion in Tanks"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-02","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"10","bibliographicVolumeNumber":"1095","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1095","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"自由表面をもつタンク内液体の運動解析の手法として液体重心の動きを追うアルゴリズムLAMPSがある。そのオリジナルプログラムにおいては液体の減衰は実験値から入力されるため,予測計算に使うには汎用性に欠けていた。本報告ではこのアルゴリズムの欠点であった減衰力の入力について,減衰を理論的に導き,その実用性を既存の試験結果により確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The dynamic behavior of liquid propellants in launch vehicles and spacecraft has been of great importance in past current generation vehicle designs. A method to theoretically estimate the viscous dissipative force from liquid propellants transient motion in tanks is present. The estimation algorithm is combined into the LAMPS(Large AMPlitude Sloshing) algorithm, where the dissipative values have been approximated from test data. Analytical predictions show excellent correlation with existing test results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1095000","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 TR-1095","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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構造力学部"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Structural Mechanics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan(NASDA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小松, 敬治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 順一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KOMATSU, Keiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMIZU, Junichiro","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr01095.pdf","filesize":[{"value":"604.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01095.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45354/files/naltr01095.pdf"},"version_id":"e8cfa2e8-ebd7-48ef-be97-83977fa7868c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Damping;  liquid;  spacecraft;  sloshing;  propellant","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":"タンク内液体の大変形時での減衰の評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"タンク内液体の大変形時での減衰の評価"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45354","relation_version_is_last":true,"title":["タンク内液体の大変形時での減衰の評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:54.592665+00:00"}