{"created":"2023-06-20T15:14:14.508829+00:00","id":44222,"links":{},"metadata":{"_buckets":{"deposit":"166384ee-7b73-4c83-9ead-75b25349718e"},"_deposit":{"created_by":1,"id":"44222","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44222"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044222","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["468428","468427","468431","468426","468424","468429","468432","468433","468434","468430","468423","468425"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Force Measurements on AGARD Calibration Model-B at Transonic Speeds in the NAL Two-Dimensional Wind Tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-08","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"12","bibliographicVolumeNumber":"639","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to investigate the capability of conducting force measurements of three-dimensional (3-D) models in NAL′s two-dimensional (2-D) wind tunnel, force measurements on AGARD calibration Model-B (Mach numbers: 0.5-1.1, Reynolds number : 3×106and 4×106). Full and half models were tested. Four different strut lengths having a circular arc cross-section and stings were used to install the full model. For the half model, a plate was installed to remove the effects of the wind tunnel′s sidewall boundary layer, as well as adding a small gap between the model and the plate to remove the effects of the plate′s boundary layer. It was shown that force measurements of 3-D models are possible in NAL′s 2-D wind tunnel, although improvements in the struts and stings are necessary to conduct tests at Mach numbers greater than 0.85.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0639000","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-639","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力性能部"},{"subitem_text_value":"航空宇宙技術研究所空力性能部"},{"subitem_text_value":"航空宇宙技術研究所空力性能部"},{"subitem_text_value":"航空宇宙技術研究所空力性能部"},{"subitem_text_value":"航空宇宙技術研究所空力性能部"},{"subitem_text_value":"航空宇宙技術研究所空力性能部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"神田, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"須谷, 記和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"馬場, 滋夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三輪, 等"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河本, 巌"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SATO, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KANDA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUDANI, Norikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"BABA, Shigeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MIWA, Hitoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMOTO, Iwao","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":"2020-01-29"}],"displaytype":"detail","filename":"naltm00639.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00639.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44222/files/naltm00639.pdf"},"version_id":"0e7ac13f-25b1-4072-9158-e21ea809a2bc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"transonic flow;  two-dimensional wind tunnel;  force measurement tests","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":"二次元風洞におけるAGARD-B標準模型の三分力試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"二次元風洞におけるAGARD-B標準模型の三分力試験"}]},"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":"44222","relation_version_is_last":true,"title":["二次元風洞におけるAGARD-B標準模型の三分力試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:00:41.289495+00:00"}