{"created":"2023-06-20T15:15:15.430677+00:00","id":45324,"links":{},"metadata":{"_buckets":{"deposit":"6981a0f6-1cf3-48ed-8570-67e103e1d8ed"},"_deposit":{"created_by":1,"id":"45324","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45324"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045324","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474124","474125","474121","474123","474126","474122"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"境界要素法を用いた亜音速流中の三次元揚力物体の非定常空力特性の計算"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"70","bibliographicVolumeNumber":"1065","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1065","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A boundary element method of unsteady compressible potential flow around lifting bodies having arbitrary configurations and harmonic oscillation motions has been developed using Green's function. Morino described the form of the integral equation relating the perturbation potential and its normal derivative. The purpose of this paper is to present a new paneling and derivative technique which can be applied to any complex configuration for evaluating the derivative of unsteady velocity potential on the surface. Numerical results for a wing-store model are presented and compared to experimental results in a subsonic flow. Good agreement has been obtained between the two.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1065000","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-1065","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空力性能部"},{"subitem_text_value":"航空宇宙技術研究所構造力学部"},{"subitem_text_value":"三菱重工業株式会社名古屋航空機製作所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Structural Mechanics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries, Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"柳沢, 三憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森田, 甫之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"巽, 重文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YANAGISAWA, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MORITA, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TATSUMI, Shigefumi","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":"naltr01065.pdf","filesize":[{"value":"3.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01065.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45324/files/naltr01065.pdf"},"version_id":"34ab972f-9340-4061-a7ff-981749dc4e04"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Calculations for Unsteady Aerodynamic Characteristics on a 3-D Lifting Body in Subsonic Flow Using Boundary Element Method","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Calculations for Unsteady Aerodynamic Characteristics on a 3-D Lifting Body in Subsonic Flow Using Boundary Element Method","subitem_title_language":"en"}]},"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":"45324","relation_version_is_last":true,"title":["Calculations for Unsteady Aerodynamic Characteristics on a 3-D Lifting Body in Subsonic Flow Using Boundary Element Method"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:41:22.304787+00:00"}