{"created":"2023-06-20T14:39:47.425069+00:00","id":6585,"links":{},"metadata":{"_buckets":{"deposit":"994cf02a-6e8c-4ccc-9df9-81d7b1eab599"},"_deposit":{"created_by":1,"id":"6585","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6585"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006585","sets":["1887:1891","9:789:1085:1087"]},"author_link":["33676","33677","33671","33675","33670","33678","33673","33674","33679","33672"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Preliminary test of stereo PIV system applied to the 6.5 m x 5.5 m low speed wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"8","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-03-004","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第67回　風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 67th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Preliminary tests of a stereo PIV system applied to a large-scale, low-speed wind tunnel are conducted. A tip vortex generated by a rectangular wing with an angle of attack and interfered flowfield between jet-engine exhaust and external flow are demonstratively measured by an off-the-shelf PIV system to examine the applicability of the stereo PIV technique to the large-scale wind tunnel and to acquire data required to determine the specifications of the system. The test results proved applicability of the stereo PIV to the large-scale, low-speed wind tunnel, while accuracy evaluation is to be done extensively in future. It was also found that the vibration of the wind tunnel has little effects on the velocity measurement accuracy while it does have effects on the location of the imaging area.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047429001","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-03-004","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"},{"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"},{"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":"加藤, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 重哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"星野, 秀雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"末永, 尚史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 輝臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Shigeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hoshino, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suenaga, Hisashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakaya, Teruomi","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":"47429001.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47429001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6585/files/47429001.pdf"},"version_id":"1d8fabd2-a849-4eb9-973b-07d8fb5e0865"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"粒子画像流速計測","subitem_subject_scheme":"Other"},{"subitem_subject":"粒子追跡流速測定","subitem_subject_scheme":"Other"},{"subitem_subject":"レーザドップラー流速計","subitem_subject_scheme":"Other"},{"subitem_subject":"流れの可視化","subitem_subject_scheme":"Other"},{"subitem_subject":"翼端渦","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"particle image velocimetry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"particle tracking velocimetry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laser doppler velocimeter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow visualization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing tip vortex","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":"航技研6.5m×5.5m低速風洞におけるステレオPIVシステム開発予備試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研6.5m×5.5m低速風洞におけるステレオPIVシステム開発予備試験"}]},"item_type_id":"5","owner":"1","path":["1087","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6585","relation_version_is_last":true,"title":["航技研6.5m×5.5m低速風洞におけるステレオPIVシステム開発予備試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:52:55.785319+00:00"}