{"created":"2023-06-20T15:08:32.123984+00:00","id":38010,"links":{},"metadata":{"_buckets":{"deposit":"63a166ef-4c5b-4637-aeae-723395bfb436"},"_deposit":{"created_by":1,"id":"38010","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38010"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038010","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431136","431133","431134","431137","431135","431140","431138","431139"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Supersonic wind tunnel testing for investigating SST inlet unstart phenomena"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"33","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第64回・第65回風洞研究会議論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 64th and 65th Workshop on Wind Tunnel Research","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"SST(次世代超音速旅客機)のインテーク不始動時にインテークから吐き出される衝撃波の挙動を明らかにすることを目的に、超音速風洞実験を実施した。インテーク不始動現象の模擬はナセル流路出口面積を制御することにより行ない、衝撃波の挙動を捕らえるために、主翼下面に取付けた非定常圧力センサによる圧力計測を行なった。本講演では、風洞試験/風試模型の概要および得られた風洞試験結果について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032235005","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 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