{"created":"2023-06-20T14:35:51.970539+00:00","id":2141,"links":{},"metadata":{"_buckets":{"deposit":"7e868263-d919-4bf4-9f2a-2547df7f810a"},"_deposit":{"created_by":1,"id":"2141","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2141"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002141","sets":["1887:1893","9:10:147:166"]},"author_link":["3703","3701","3697","3695","3699","3698","3700","3696","3694","3702"],"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 2 m x 2 m transonic 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-07-033","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":"JAXA2m×2m遷音速風洞では、これまでいくつかの風洞壁境界修正法が検討されてきたが実用化されたものは無く、現在境界修正を施さない空力データをユーザに提供している。そこで、より信頼性の高いデータをユーザに提供することを目的として、NASAの風洞で実用化されているレストリクションパラメータを取り入れ、風洞壁面での境界条件を簡単化したパネル法境界修正法を参考として、風洞壁静圧を使用せず揚力係数と抵抗係数から模型揚力および後流ブロッケージを表すダブレット強さを推算し風洞壁境界修正量を求める手法を開発した。また、本境界修正法の検証は、鏡像法との比較によるプログラムコード自体の検証、および検証風洞試験で計測した風洞壁擾乱速度分布と本手法による計算擾乱速度分布の比較により行い、本境界修正法は信頼性のあることを確認した。さらに、計算モデルの近似において、揚力の楕円分布近似や後流の上下方向位置および縮流効果は、境界修正量に有意な影響を与えないことを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the JAXA transonic wind tunnel, some wall interference correction methods were investigated in the past, but they were not made practicable. And so, we have offered uncorrected wind tunnel data to users. We developed the wall interference correction method to improve the reliability of the wind tunnel data and to offer them to users, in which we used the measured lift and drag coefficient and the restriction parameter in the panel method that was used in the NASA wind tunnel. The validity of this method was checked by the comparison with the analytical method of images and the comparison with the wind tunnel wall perturbation velocity distributions measured in the validity wind tunnel test. As a result, we confirmed that this method was practical and the approximation of the elliptical lift lord distribution and the wake position did not have a significant influence on the correction quantity.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063885000","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-07-033","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":"小池, 陽"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"香西, 政孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"森田, 義郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hidaka, Akiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuchiishi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koike, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kozai, Masataka","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":"63885000.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63885000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2141/files/63885000.pdf"},"version_id":"6fd756bc-1a55-46ee-b1b3-e24b943fe3a6"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面干渉","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":"壁面圧","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型","subitem_subject_scheme":"Other"},{"subitem_subject":"静圧","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"境界条件","subitem_subject_scheme":"Other"},{"subitem_subject":"速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"補正","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall interference","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":"wall pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"correction","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":"パネル法による遷音速風洞境界修正法の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"パネル法による遷音速風洞境界修正法の開発"}]},"item_type_id":"3","owner":"1","path":["166","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2141","relation_version_is_last":true,"title":["パネル法による遷音速風洞境界修正法の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:27:57.239358+00:00"}