{"created":"2023-06-20T14:39:44.950580+00:00","id":6527,"links":{},"metadata":{"_buckets":{"deposit":"e4cae41a-dcd3-494e-a00d-f2f04d0681a6"},"_deposit":{"created_by":1,"id":"6527","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6527"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006527","sets":["1887:1891","9:789:1067:1077"]},"author_link":["33326","33324","33325","33322","33321","33323"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Correction of flutter boundary of non-planar wing using measured local Mach number"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"8","bibliographicVolumeNumber":"JAXA-SP-04-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第69回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 69th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For the anti-symmetric flutter speeds of a tip-fin-shaped reentry space vehicle model, numerical predictions using Doublet-Point Method (DPM) have been different from experimental results in a part of lower supersonic region. The cause of the discrepancy is suspected to be that the local flow over the wing differs from the free stream. Instead of free stream Mach numbers, measured local Mach numbers are adopted for flutter boundary analyses, and the corrected numerical results show good agreement with experimental ones. Therefore, it is made clear that the correction by local Mach numbers improves the accuracy of the flutter boundary.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048061002","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-04-008","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"甲斐, 高志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 俊哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kai, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Toshiya","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":"2020-01-16"}],"displaytype":"detail","filename":"48061002.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48061002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6527/files/48061002.pdf"},"version_id":"0d2d94db-7f0b-4a6e-8bff-6eaa798983bf"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"DPM","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ境界","subitem_subject_scheme":"Other"},{"subitem_subject":"翼","subitem_subject_scheme":"Other"},{"subitem_subject":"低超音速領域","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入機","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力測定","subitem_subject_scheme":"Other"},{"subitem_subject":"DPM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter boundary","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low supersonic region","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure measurement","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"計測局所マッハ数による非平面翼のフラッタ限界値補正","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"計測局所マッハ数による非平面翼のフラッタ限界値補正"}]},"item_type_id":"5","owner":"1","path":["1077","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6527","relation_version_is_last":true,"title":["計測局所マッハ数による非平面翼のフラッタ限界値補正"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:54:06.654624+00:00"}