{"created":"2023-06-20T15:10:18.502293+00:00","id":39893,"links":{},"metadata":{"_buckets":{"deposit":"ecb8f178-bc87-4ecd-be94-3939c1923c02"},"_deposit":{"created_by":1,"id":"39893","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39893"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039893","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["445502","445499","445498","445500","445503","445501"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The blockage correction methods for low-speed wind tunnel testing on delta wings"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"707","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"相似で翼面積の異なる2つのデルタ翼模型により、低速風洞試験を実施して閉塞修正の方法を検討した。扱った閉塞修正方法は、Maskellの伴流閉塞修正を含む古典的方法と、進藤により提案された単純化した方法である。単純化した閉塞修正の係数式の理論的な意味を表わすために、知られている古典的閉塞修正の係数式を変形した。その結果として、古典的閉塞修正係数式は単純化した閉塞修正係数式を中に含み、残りの余剰項は正と負の項が差し引きしあって小さな値になることを示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The blockage correction methods are investigated for low-speed wind tunnel testing on two geometrically similar delta wings with different reference areas. The blockage correction methods used are the classical Maskell method and the simplified tunnel correction method proposed by Shindo. The expression of blockage correction factors in the known classical method is modified to clarify the theoretical meaning of the expression of blockage correction factors in the simplified method. It was concluded, consequently, that the expression of blockage correction factors in the classical method implicates one in the simplified method, and also the total sum of the remainder terms are small due to the offsets of the plus and minus terms.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000871000","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 TM-707","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":"0452-2982","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":"AN00314334","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 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"奥山, 政広"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okuyama, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00707.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00707.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39893/files/naltm00707.pdf"},"version_id":"2118fec7-6608-4f71-85a1-78bc08893dc1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"閉塞修正法","subitem_subject_scheme":"Other"},{"subitem_subject":"デルタ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"閉塞修正係数","subitem_subject_scheme":"Other"},{"subitem_subject":"Maskell法","subitem_subject_scheme":"Other"},{"subitem_subject":"進藤法","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"伴流","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"blockage correction method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blockage correction factor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Maskell method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Shindo method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wake flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristics","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":"閉塞修正方法の検討:デルタ翼模型の低速風洞試験の実施と閉塞修正係数式の変形","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"閉塞修正方法の検討:デルタ翼模型の低速風洞試験の実施と閉塞修正係数式の変形"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39893","relation_version_is_last":true,"title":["閉塞修正方法の検討:デルタ翼模型の低速風洞試験の実施と閉塞修正係数式の変形"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:31.037344+00:00"}