{"created":"2023-06-20T15:07:50.084039+00:00","id":37199,"links":{},"metadata":{"_buckets":{"deposit":"547acb2d-b66c-432a-b317-fb7f625cea5f"},"_deposit":{"created_by":1,"id":"37199","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37199"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037199","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479511","479502","479512","479506","479504","479509","479510","479513","479503","479507","479505","479508"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Installation of the high speed pressure acquisition system in the NAL 1 m x 1 m supersonic wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"208","bibliographicPageStart":"195","bibliographicVolumeNumber":"38","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"高速多点圧力計測システムZOC HyScan2000(スキャニバルブ社)がNALの1m×1m超音速風洞に1995年度末に設置された。このシステムは約1年を要した準備作業ののち、1997年5月から本格運用に入った。本報告は、従来の機械式圧力走査器との比較でこのシステムの性能評価を述べる。この新システムは、満足できる精度を保ちながら、データ生産性を飛躍的に向上させた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The high speed pressure acquisition system by 'ZOC HyScan 2000' (Scanivalve Corp.) was installed in the NAL 1 m x 1 m supersonic wind tunnel in the end of FY 1995. The system has been actively in operation since May 1997, after some preparation works consuming about one year. The performance of the system is examined in this report, comparing with the conventional mechanical pressure scanner. The new system yields a dramatic rise in data productivity while the accuracy is kept satisfied.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434017","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: NAL SP-38","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","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"},{"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"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"浜本, 滋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"楯, 篤志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原, 亘利"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 洋治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamamoto, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tate, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Nobutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Yoji","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0038017.pdf","filesize":[{"value":"3.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37199/files/nalsp0038017.pdf"},"version_id":"aaa25478-9907-4fee-8b00-5a8ef3e2b901"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高速多点圧力計測装置","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力センサ","subitem_subject_scheme":"Other"},{"subitem_subject":"電子式圧力走査器","subitem_subject_scheme":"Other"},{"subitem_subject":"EPS","subitem_subject_scheme":"Other"},{"subitem_subject":"計測効率","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布測定","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞特性","subitem_subject_scheme":"Other"},{"subitem_subject":"計測精度","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed pressure acquisition system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure sensor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electronic pressure scanner","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"EPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"data productivity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement accuracy","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1m×1m超音速風洞における高速多点圧力計測装置の導入","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研1m×1m超音速風洞における高速多点圧力計測装置の導入"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37199","relation_version_is_last":true,"title":["航技研1m×1m超音速風洞における高速多点圧力計測装置の導入"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:36.622052+00:00"}