{"created":"2023-06-20T15:07:46.594246+00:00","id":37139,"links":{},"metadata":{"_buckets":{"deposit":"e2a3bae8-6af2-4540-bd0c-01ffdc7fa644"},"_deposit":{"created_by":1,"id":"37139","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37139"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037139","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479094","479093","479092","479095"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Role of CFD in aeronautical engineering. 15: Aerodynamic design of an SST wing"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"86","bibliographicPageStart":"81","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":"NAL(航空宇宙技術研究所)の小型無人実験機の翼をL/D(揚抗)比を高めるように設計した。特に、全抗力のほとんど半分を占める翼部分の摩擦抗力を低減するように設計した。この目的のため、UG3(3次元非構造格子CFD(数値流体力学)ソルバ)およびSALLY(3次元層流境界層安定性解析コード)を用いて、出来るだけ層流を保つようにして、翼部分を設計した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The wing of the sub-scaled unmanned experimental aircraft of NAL is designed to improve the L/D (Lift to Drag) ratio. The wing section is designed especially to reduce skin friction drag, which amounts to nearly half of the total drag. For this purpose, the wing section was designed to remain laminar flow as far as possible, using UG3 (3D (Three Dimensional) Unstructured Grid CFD (Computational Fluid Dynamics) solver) and SALLY (3D laminar boundary layer stability analysis code).","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433013","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":"川崎重工業"},{"subitem_text_value":"川崎重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"生越, 博景"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogoshi, Hirokage","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Eiji","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":"nalsp0037013.pdf","filesize":[{"value":"758.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37139/files/nalsp0037013.pdf"},"version_id":"83e90b33-2a1c-472e-80d7-9e62aa519179"}]},"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":"主翼空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"小型高速実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力低減","subitem_subject_scheme":"Other"},{"subitem_subject":"摩擦抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造格子","subitem_subject_scheme":"Other"},{"subitem_subject":"層流境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"低アスペクト比翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼胴形状","subitem_subject_scheme":"Other"},{"subitem_subject":"逆設計法","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":"main wing aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"subscaled high speed experimental aircraft","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":"drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"friction drag","subitem_subject_language":"en","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":"unstructured grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low aspect ratio wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing body configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse design method","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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