{"created":"2023-06-20T15:07:45.709960+00:00","id":37126,"links":{},"metadata":{"_buckets":{"deposit":"daded0c0-0940-4357-90be-af0b4661bceb"},"_deposit":{"created_by":1,"id":"37126","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37126"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037126","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479020","479019"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Proceedings of the 15th NAL Symposium on Aircraft Computation Aerodynamics"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"343","bibliographicPageStart":"1","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":"CFD(数値流体力学)に関する次の主題を論じている。(1)SST(超音速輸送)、小型高速実験機、SSTの主翼空力設計、ナセルのブリード流/バイパス流効果、(2)高エンタルピー流れ、空力加熱の化学反応モデル、衝撃波誘起非定常空力加熱、(3)航空エンジン/宇宙推進、航空機エンジン内の3次元非定常流れ解析、(4)回転翼、ヘリコプタ・メインロータ周りの流れ、ロータCFDコードの開発、および(5)乱流、圧縮性流体の乱流、平行平板間の乱流熱伝達。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The following subjects on CFD (Computational Fluid Dynamics) are discussed: (1) SST (Supersonic Transport), scaled high-speed experimental aircraft, aerodynamic design of a SST wing, bleed and bypass effects of nacelles; (2) high enthalpy flows, chemical reaction model of aerodynamic heating, shock wave induced unsteady aerodynamic heating; (3) aircraft engine/space propulsion, three dimensional unsteady flow analysis in turbomachinery; (4) rotor, flowfields around main rotor,  development of rotor CFD codes, and (5) turbulence, turbulence of compressible flows, turbulent heat transfer in a channel between parallel plates.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433000","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":"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":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"航空宇宙技術研究所"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"National Aerospace Laboratory","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":"nalsp00037.pdf","filesize":[{"value":"50.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp00037.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37126/files/nalsp00037.pdf"},"version_id":"d76b9df0-a72e-4fb1-8b0d-ea29a5176672"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_scheme":"Other"},{"subitem_subject":"数値風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"液滴燃焼器内部流","subitem_subject_scheme":"Other"},{"subitem_subject":"ヘリコプタ","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計コード","subitem_subject_scheme":"Other"},{"subitem_subject":"スクラムジェットインレット","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波乱流境界層干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"ランプインジェクタ","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速混合","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Numerical Wind Tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"droplet combustor internal flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"helicopter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet inlet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave turbulent boundary layer interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ramp injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic mixing","subitem_subject_language":"en","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":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","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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