{"created":"2023-06-20T14:39:47.252875+00:00","id":6581,"links":{},"metadata":{"_buckets":{"deposit":"31e13cc8-9083-463a-b408-484256eef174"},"_deposit":{"created_by":1,"id":"6581","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6581"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006581","sets":["1887:1891","9:789:1085:1086"]},"author_link":["33655","33656","33654","33657"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"第2報"}]},"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flow quality test results of NAL 1 m supersonic wind tunnel"},{"subitem_alternative_title":"Second Report"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"17","bibliographicPageStart":"11","bibliographicVolumeNumber":"JAXA-SP-03-005","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第68回　風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 68th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1999年から行われた、NAL 1m×1m超音速風洞の改修工事および改修後の気流特性については2001年5月の第66回風洞研究会議で工事の概要および主要なマッハ数6点に対するマッハ数分布計測結果が報告されている。航空宇宙技術研究所ではその後も詳細な気流特性確認作業を継続し、通風中に発生するシュリーレン窓の段差がマッハ数分布に悪影響を及ぼしていることを発見、これを修正し、現在では常用される全てのマッハ数について要求値ΔM(sub max)＜±0.5％が達成されていることを確認した。さらにAGARD-B標準模型による気流偏向特性試験の結果、気流の傾きは全マッハ数範囲で要求値の±0.1度以内であること、側壁付近で実施した総圧変動計測予備試験の結果、気流の乱れは改修前に比べ、オーバーオールの変動で約1/3に低減していることを確認した。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047430002","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-03-005","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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鈴木, 教雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Norio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Mitsunori","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":"47430002.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47430002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6581/files/47430002.pdf"},"version_id":"bd6d0854-0f16-4c3f-9ff7-b91aa8220998"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"気流特性","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力変動","subitem_subject_scheme":"Other"},{"subitem_subject":"気流偏向","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic 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":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure variation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow deflection","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":"NAL 1m×1m超音速風洞気流特性試験結果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"NAL 1m×1m超音速風洞気流特性試験結果"}]},"item_type_id":"5","owner":"1","path":["1086","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6581","relation_version_is_last":true,"title":["NAL 1m×1m超音速風洞気流特性試験結果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:52:59.890849+00:00"}