{"created":"2023-06-20T15:15:21.045924+00:00","id":45425,"links":{},"metadata":{"_buckets":{"deposit":"d6239e74-eb1d-4891-8fb4-0817d66d6f10"},"_deposit":{"created_by":1,"id":"45425","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45425"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045425","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474730","474729","474727","474726","474728","474725"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Self-illumination Correction for Pressure Sensitive Paints on Airplane Models in Wind Tunnel Testing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"20","bibliographicVolumeNumber":"1441","bibliographic_titles":[{"bibliographic_title":"独立行政法人航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1441","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機形態の風洞試験において感圧塗料により圧力を計測する際の問題の一つとして，翼面からの光を計測する際，胴体面からの光が翼面で反射した分が含まれてしまうという問題がある。本報告では，Ruytenの報告を基に一般的な航空機模型の感圧塗料試験に適用可能な計測手法とデータ処理プログラムを開発した。本手法では，感圧塗料の反射係数を一つのスカラー量に定めて風洞試験とは別に計測して，反射の影響を数値的に除去する。本手法を2つの平板を組み合わせた形状に適用したところ，本研究で用いた塗料PtOEP-GP197の反射係数の計測値は0.75であり，その値を用いた反射補正によって反射の影響を取り除くことができることがわかった。本手法をMU-300模型の風洞試験に適用したが，反射の影響が小さかったため，反射補正の効果はわずかであった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"One of the potential problems in applying pressure sensitive paints to a wing-body model is self-illumination of the model. A theoretical model of self-illumination correction by W. M. Ruyten was applied to two, square, painted samples and a wind tunnel test of the MU-300 model. The spatially averaged reflection coefficient of 0.75 was determined for a pressure sensitive paint PtOEP-GP197 by measurement on the two, square, painted samples at a range of included angles. As a result, the applicability of the self-illumination correction method was validated. The self-illumination effect on the MU-300 model was so small that the effect of the self-illumination correction was little.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1441000","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 TR-1441","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":"1347-4588","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":"AN00311347","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流体科学研究センター"},{"subitem_text_value":"航空宇宙技術研究所流体科学研究センター"},{"subitem_text_value":"航空宇宙技術研究所流体科学研究センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fluid Science Research Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Science Research Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Science Research Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"杉浦, 裕樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"飯島, 由美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浅井, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUGIURA, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IIJIMA, Yoshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ASAI, Keisuke","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":"naltr0001441.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001441.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45425/files/naltr0001441.pdf"},"version_id":"a5d33ef4-5a9f-45a8-94d8-aa6754255cb5"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Pressure Sensitive Paint; Self-Illumination Correction; Reflection Coefficient","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":"航空機風洞試験における感圧塗料の反射補正","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空機風洞試験における感圧塗料の反射補正"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45425","relation_version_is_last":true,"title":["航空機風洞試験における感圧塗料の反射補正"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:39:42.726633+00:00"}