{"created":"2023-06-20T15:07:46.459245+00:00","id":37137,"links":{},"metadata":{"_buckets":{"deposit":"c8e8ca73-3336-4619-ba01-e9292941fe50"},"_deposit":{"created_by":1,"id":"37137","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37137"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037137","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479087","479083","479085","479086","479084","479082"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation with bleed and bypass effects of nacelles"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"74","bibliographicPageStart":"69","bibliographicVolumeNumber":"37","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_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 12-13 Jun. 1997 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 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"超音速輸送機(SST)は、衝撃波形を利用するために、通常、機体とエンジンナセル間の統合化を考慮して空力設計される。しかし、実用では抽気(ブリード)流およびバイパス流をナセルから吹き出す。それ故、空力干渉の把握が必要となる。ここでは、ナセルからの吹き出しによる空力干渉現象をナビエ・ストークスソルバにより解析したので報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Supersonic transport is usually aero-designed with the consideration of the integration between airframe and engine nacelles to utilized the shock wave from them. But the bleed and bypass flow is blown outside from nacelles in the view points of the practical use. Therefore it is necessary to catch the aerodynamic interference. It is here reported that the aero-interference phenomena by blowing from nacelles are obtained by Navier-Stokes solver.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433011","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-37","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":"日本航空機開発協会"},{"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":"Japan Aircraft Development Corporation"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前川, 昭二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maekawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","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":"nalsp0037011.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37137/files/nalsp0037011.pdf"},"version_id":"8aa38f54-136e-46c9-8492-aae013ebe6fc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"空力統合化設計","subitem_subject_scheme":"Other"},{"subitem_subject":"機体ナセル空力干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"抽気流","subitem_subject_scheme":"Other"},{"subitem_subject":"バイパス流","subitem_subject_scheme":"Other"},{"subitem_subject":"吹出し","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスソルバ","subitem_subject_scheme":"Other"},{"subitem_subject":"剥離衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"計算格子生成","subitem_subject_scheme":"Other"},{"subitem_subject":"抽気バイパス効果","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic integration design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe nacelle aerodynamic interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bleed flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bypass flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blowing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes solver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separation shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift to drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calculation grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bleed bypass effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","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":"SSTにおけるナセルのブリード流/バイパス流を考慮した数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"SSTにおけるナセルのブリード流/バイパス流を考慮した数値シミュレーション"}]},"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":"37137","relation_version_is_last":true,"title":["SSTにおけるナセルのブリード流/バイパス流を考慮した数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:25:09.739230+00:00"}