{"created":"2023-06-20T15:10:11.963268+00:00","id":39794,"links":{},"metadata":{"_buckets":{"deposit":"16ba9914-48cc-45cc-8d1c-e9ffe38ef926"},"_deposit":{"created_by":1,"id":"39794","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39794"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039794","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["444444","444445","444447","444446","444443","444442"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The flow characteristics of the repaired NAL's 1 m x 1 m supersonic wind tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"1","bibliographicVolumeNumber":"694","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航技研の1m×1m超音速風洞のノズルを修理した。修理したノズルは可撓式であり、マッハ数1.4-4.2の範囲で任意のマッハ数に設定可能なものである。この修理工事によってノズル形状を修正すると共に老朽化した部材のオーバーホールを実施した。また、修理前後の測定部流れの傾き角およびマッハ数分布測定ならびにAGARD標準模型Bによる3分力試験を実施し、概ね新設時の特性を持っていることを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The nozzle of the 1 m x 1 m supersonic wind tunnel of the National Aerospace Laboratory was partially repaired. After the measurement of the nozzle shape dimensions by using a laser measuring instrument, the shape was adjusted to approach to the designed dimensions. The rubber seal was exchanged to a new one. After the repair, the inclination of the flow in the test section was measured using a five hole Pitot tube and the AGARD (Advisory Group for Aerospace Research and Development)-B standard model. Mach number distributions along the nozzle and cross-section of the test section were measured by the static pressures and the Pitot tube. The flow characteristics are close to the one initially designed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000555000","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 TM-694","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":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00694.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00694.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39794/files/naltm00694.pdf"},"version_id":"5df0512d-cb08-49ec-98a3-e835e802ce3f"}]},"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":"AGARD標準模型B","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"気流特性","subitem_subject_scheme":"Other"},{"subitem_subject":"気流傾斜角","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数分布","subitem_subject_scheme":"Other"},{"subitem_subject":"3分力試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD B standard model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow inclination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three component test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind nozzle","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"航技研1m×1m超音速風洞のノズル修理後の気流特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研1m×1m超音速風洞のノズル修理後の気流特性"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39794","relation_version_is_last":true,"title":["航技研1m×1m超音速風洞のノズル修理後の気流特性"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:14.165511+00:00"}