{"created":"2023-06-20T15:11:38.432470+00:00","id":41329,"links":{},"metadata":{"_buckets":{"deposit":"4fefcde2-f092-4257-8f11-1a70a6bba931"},"_deposit":{"created_by":1,"id":"41329","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41329"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041329","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489499","489493","489498","489491","489495","489492","489496","489497","489494","489490"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation on 2D airfoil stall prediction using CASPER"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"156","bibliographicPageStart":"151","bibliographicVolumeNumber":"46","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"この論文では、CASPER(航空機性能評価システム)の2次元翼型失速予測への応用について示した。これは、国内航空機製造会社との共同で、TRDIJDA(防衛庁技術研究本部)が開発した。異なる失速特性を持った3種類の翼型周りの流れ場について、RANS(レイノルズ平均ナビエ-ストークス)計算を行った。ここで、非構造多重格子法とスパラート-アルマラス1方程式乱流モデルも用いた。計算結果は、実験の圧力分布と低仰角での揚力係数と良い一致を示し、Cl(sub max)(最大揚力係数)と仰角予測の可能性を示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents the applications of CASPER (Computational Aerodynamic System for Performance Evaluation and Research) to 2D (two dimensional) airfoil stall prediction, developed by TRDIJDA (Technical Research and Development Institute of Japan Defense Agency) in collaboration with domestic aircraft manufactures. The RANS (Reynolds-Averaged Navier-Stokes) computations for flows around three airfoils were carried out, which have different stall characteristics, using unstructured grid method together with Spalart-Allmaras one-equation turbulence model. The computational results show good agreement with the experimental pressure distribution and Lift coefficient for low angles of attack, and indicate the potential to predict Cl(sub max) and the angle of attack.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635028","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 SP-46","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":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"防衛庁 技術研究本部"},{"subitem_text_value":"防衛庁 技術研究本部"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"}]},"item_3_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":"Japan Defense Agency Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Japan Defense Agency Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"竹中, 啓三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"酒田, 威志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沖, 良篤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中尾, 雅弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"増永, 晶久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takenaka, Keizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oki, Yoshiatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakao, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masunaga, Akihisa","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":"nalsp0046028.pdf","filesize":[{"value":"931.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41329/files/nalsp0046028.pdf"},"version_id":"70db9b69-c840-4078-9c8d-bd87fe278969"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"失速特性","subitem_subject_scheme":"Other"},{"subitem_subject":"失速予測","subitem_subject_scheme":"Other"},{"subitem_subject":"RANS","subitem_subject_scheme":"Other"},{"subitem_subject":"スパラート-アルマラス・モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"仰角","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造多重格子法","subitem_subject_scheme":"Other"},{"subitem_subject":"CASPER","subitem_subject_scheme":"Other"},{"subitem_subject":"TRDIJDA","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"計算結果","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"aerofoil section","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall prediction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RANS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Spalart Allmaras model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstructured grid method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CASPER","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TRDIJDA","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational result","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional airfoil","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":"CASPERを用いた翼型失速特性シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"CASPERを用いた翼型失速特性シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41329","relation_version_is_last":true,"title":["CASPERを用いた翼型失速特性シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:04.300288+00:00"}