{"created":"2023-06-20T15:08:20.683139+00:00","id":37768,"links":{},"metadata":{"_buckets":{"deposit":"5fb50009-6929-48b8-a085-9d860ed6abd5"},"_deposit":{"created_by":1,"id":"37768","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37768"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037768","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482893","482895","482896","482894"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis on wing/nacelle interference using overlapped grid method"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"52","bibliographicPageStart":"47","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11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 11th 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 10-11 Jun. 1993 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 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"輸送機形態に関する主翼/ナセル干渉の数値解析を行った。干渉抵抗を減らすためのリプレットと称する小翼の形状をいくつか設計した。リプレットは、ナセルファンカウル後縁の上方やや下流のパイロン両側に取りつけられ、干渉領域における流れを制御する。遷音速巡航条件において3次元オイラー方程式の解を計算した。重ね合せ格子法を用いた流れ場解析コードを開発し、翼-ナセル/リプレットまわりの流れ場の計算に適用した。計算結果は翼面静圧分布に対するリプレットの効果を明らかにし、重ね合せ格子法が複雑な形状の場合を解析するのに効果的であることを示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A numerical study was carried out on wing/nacelle interference for transonic transports. To reduce the interference drag, some shapes of small wings, Liplets, were designed. Liplet is a wing installed on both sides of the pylon just downstream of the upper part of the nacelle fan cowl trailing edge, to control the flow in the interference region. Three dimensional Euler calculation was carried out at transonic cruise condition. A flow analysis code using overlapped grid method was developed and successfully applied to calculate the flow field around the wing-nacelle and liplet configuration. The result shows the effect of the liplet to the wing surface pressure, and indicates the overlapped grid method is efficient to analyze such a complicated geometry.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171008","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-22","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":"富士重工業"},{"subitem_text_value":"日本航空機開発協会"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"谷, 泰寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 完一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Amano, Kanichi","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":"nalsp0022008.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37768/files/nalsp0022008.pdf"},"version_id":"59c7211d-d27e-4dae-859c-43a92a6c074c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"主翼ナセル干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"空力干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード開発","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー方程式数値解法","subitem_subject_scheme":"Other"},{"subitem_subject":"重ね合せ格子法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流れ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"機体エンジン統合","subitem_subject_scheme":"Other"},{"subitem_subject":"主翼ナセル風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"動力効果付き風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"リプレット","subitem_subject_scheme":"Other"},{"subitem_subject":"干渉抵抗軽減","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD応用","subitem_subject_scheme":"Other"},{"subitem_subject":"計算空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"wing nacelle interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler equation solution method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"overlapped grid method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine airframe integration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing nacelle wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"power effect simulation wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"liplet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interference drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD application","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Overlapped　Gridによる翼ナセル干渉の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Overlapped　Gridによる翼ナセル干渉の数値解析"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37768","relation_version_is_last":true,"title":["Overlapped　Gridによる翼ナセル干渉の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:52.323579+00:00"}