{"created":"2023-06-20T14:35:52.278250+00:00","id":2148,"links":{},"metadata":{"_buckets":{"deposit":"fb6bb2c1-ff7c-43d9-9804-e661c02f5288"},"_deposit":{"created_by":1,"id":"2148","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2148"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002148","sets":["1887:1893","9:10:147:174"]},"author_link":["3746","3744","3743","3741","3747","3740","3742","3749","3748","3745"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Wall interference correction by the panel method for the JAXA low speed wind tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-07-026","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"大型で高い揚力を発生する高揚力装置模型の低速風洞試験においては、風洞壁の空力干渉が大きくなる為、古典的な風洞壁境界修正法では空力係数の修正誤差が大きくなり、風洞試験データの信頼性が損なわれる。そこで、風洞試験で得られた揚力係数と、同時に計測した風洞壁面での静圧計測データを利用した風洞壁境界修正法を開発し、風洞試験データの信頼性を向上させることを試みた。また、開発した風洞壁境界修正法を、大小2種の相似矩形翼模型による風洞試験データに適用し、境界修正後の空力係数が一致することからその妥当性を検証した。さらに、検証の過程で、大型で高い揚力を発生する模型の場合、模型による風洞壁面での擾乱速度の取り扱いは、流れ方向に加え垂直成分も考慮する方が修正データの信頼性が増すことを明らかにした。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In low-speed wind tunnel tests for a large-scale high-lift device model, the effect of wall interference is significant and the use of a classical wall interference correction technique becomes dubious. In this report, an attempt has been made to improve the reliability of wind tunnel data by using panel method together with the lift coefficient of the model and static pressure data on the tunnel wall. The method is then applied to a low-speed wind tunnel test using small and large rectangular wing models and the validity is examined. It has been found that velocity component perpendicular to the flow should be included to improve the accuracy of data in calculating the perturbation velocity on the wall.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063941000","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: JAXA-RR-07-026","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","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":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部　風洞技術開発センター"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部　事業推進部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部　風洞技術開発センター"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部　風洞技術開発センター"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部　風洞技術開発センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Program Management and Integration Department, Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"日高, 亜希子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"口石, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森田, 義郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hidaka, Akiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuchiishi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Morita, Yoshio","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":"2020-01-15"}],"displaytype":"detail","filename":"63941000.pdf","filesize":[{"value":"1.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63941000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2148/files/63941000.pdf"},"version_id":"1b9c9d23-1f7f-431b-91bc-63027b593199"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"壁面干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞壁","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面圧","subitem_subject_scheme":"Other"},{"subitem_subject":"静圧","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力装置","subitem_subject_scheme":"Other"},{"subitem_subject":"空力干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"補正","subitem_subject_scheme":"Other"},{"subitem_subject":"境界条件","subitem_subject_scheme":"Other"},{"subitem_subject":"レイノルズ数","subitem_subject_scheme":"Other"},{"subitem_subject":"wall interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel wall","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high-lift device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"correction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds number","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":"パネル法による低速風洞境界修正法の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"パネル法による低速風洞境界修正法の開発"}]},"item_type_id":"3","owner":"1","path":["174","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2148","relation_version_is_last":true,"title":["パネル法による低速風洞境界修正法の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:27:50.839157+00:00"}