{"created":"2023-06-20T15:08:32.475926+00:00","id":38017,"links":{},"metadata":{"_buckets":{"deposit":"950e97f1-f4c4-4acf-9ee5-6ba62c445862"},"_deposit":{"created_by":1,"id":"38017","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38017"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038017","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431186","431187","431189","431183","431190","431185","431191","431193","431192","431194","431184","431188"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic heating measurement by infrared camera system"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"111","bibliographicPageStart":"103","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":"航空宇宙技術研究所の大型極超音速風洞では、空力加熱測定を赤外線カメラを用いて行っている。この赤外線カメラによる空力加熱測定法は、従来の離散的なセンサによる測定法に比べ、機体全体にわたる空力加熱を2次元的な面情報として捉えられるため、局所的なピーク加熱も捕捉できる点で優れている。また、これまで定量測定精度の問題が指摘されていたが、誤差量の見積もり、補正方法の確立、3次元マッピングソフトウェアの開発、従来型のセンサとの比較試験などを行い、総合的な測定精度として10％以内の測定が可能であることを確認した。赤外線カメラによる空力加熱測定法は、極超音速風洞における空力加熱測定の実用的なシステムとしてほぼ確立した。ここでは、赤外線カメラによる空力加熱測定法の概要と定量測定精度を高めるために行った誤差の検討と補正法、センサとの比較試験などについて報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032235012","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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