{"created":"2023-06-20T15:14:13.338682+00:00","id":44198,"links":{},"metadata":{"_buckets":{"deposit":"bac4fb86-d0e9-4b3a-bb84-c10558f58c05"},"_deposit":{"created_by":1,"id":"44198","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44198"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044198","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["468266","468259","468270","468247","468262","468269","468268","468252","468265","468257","468249","468258","468261","468245","468264","468250","468260","468254","468253","468255","468251","468267","468246","468263","468248","468256"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ATPブレードの研究(I): 薄翼の遷音速二次元風洞試験"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-11","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"48","bibliographicVolumeNumber":"615","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":"Two-dimensional transonic wind tunnel tests of thin airfoils were made as a part of aerodynamic research on propeller blades for advanced turboprop engines. The test airfoils were NACA-16-202 and NACA16-204 which were developed as airfoils for conventional propeller systems at NACA in 1934. The Reynolds number is 8×106. The Mach number was varied from 0.6 to 1.0 and angles of attack from -10 to +16. In addition, vibration characteristics were measured and analyzed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0615000","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-615","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 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