{"created":"2023-06-20T15:08:17.270895+00:00","id":37698,"links":{},"metadata":{"_buckets":{"deposit":"e35ea39c-4cc8-4109-9317-181e818c3aff"},"_deposit":{"created_by":1,"id":"37698","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37698"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037698","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482561","482559","482563","482562","482558","482556","482560","482554","482555","482557"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of airfoil for helicopter blade at high angle of attack using Navier-Stokes code"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"68","bibliographicPageStart":"63","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 10-12 Jun. 1992 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ヘリコプタ用翼型の高迎角時の流れ場をシミュレートする手法を開発する目的で、ナビエ・ストークスコードを用いた数値解析を行った。その結果を実験データと比較し、高迎角における流れ場のシミュレーションの課題を調べた。格子を後縁領域に集中させることが重要であると判明した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical analysis using Navier-Stokes code is conducted in order to develop the method to simulate flow fields around helicopter airfoils at high angle of attack. The results are compared with experimental data to investigate the subject for the simulation of the flow fields at high angle of attack. Based on the investigation, the effect of grid system is examined. It is shown that the concentration of the grid at the trailing edge is important.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168012","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 SP-19","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"足立, 直人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石黒, 満津夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中尾, 雅弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"廣瀬, 直喜"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Adachi, Naohito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishiguro, Mitsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakao, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirose, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Mamoru","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0019012.pdf","filesize":[{"value":"456.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37698/files/nalsp0019012.pdf"},"version_id":"2fdea56e-e4ef-4d68-85b4-e86e2f10f099"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ヘリコプタブレード","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス解法プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD性能","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学性能","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"高レイノルズ数風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"翼型試験データ","subitem_subject_scheme":"Other"},{"subitem_subject":"計算格子効果","subitem_subject_scheme":"Other"},{"subitem_subject":"後縁領域格子分解能","subitem_subject_scheme":"Other"},{"subitem_subject":"後縁流れ特性","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high Reynolds number wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational grid effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trailing edge region grid resolution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"trailing edge flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","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":"conference 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