{"created":"2023-06-20T15:07:24.950695+00:00","id":36789,"links":{},"metadata":{"_buckets":{"deposit":"648b5258-504e-4db4-9f4e-b0e66d14af69"},"_deposit":{"created_by":1,"id":"36789","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36789"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036789","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477627","477625","477630","477629","477626","477628"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of the flowfield around an oscillating wing in transonic range"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"120","bibliographicPageStart":"115","bibliographicVolumeNumber":"30","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 7-9 Jun. 1995 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 7-9 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"空力弾性の分野では、従来、空力弾性の予測には非粘性の非定常空気力学が用いられてきた。最近ではスーパーコンピュータの進歩を考慮し、振動翼周りの非定常流れ場のNavier-Stokes方程式ベースの数値シミュレーションが一般的になった。振動翼周りの非定常Navier-Stokes方程式を解く計算機コードを開発した。本コードはBeam-Warming ADI法をベースとし、ダイナミック格子形成システムと連結する。ここでは薄翼で低アスペクト比の振動翼に本コードを適用する場合の統合定式化について述べた。コンピュータの計算結果はNALの2m遷音速風洞での試験データと比較検討した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the field of aeroelasticity, inviscid unsteady aerodynamics have traditionally been used to predict aeroelastic phenomena. However, thanks to the recent advance of supercomputer, numerical simulation of unsteady flowfield around an oscillating wing based on the Navier-Stokes equations has become popular. Recently a computer code which is capable of solving unsteady Navier-Stokes equations around oscillating wings was developed. The code is based on the Beam-Warming ADI (Alternating Direction Implicit) method combined with a dynamic grid system. This paper describes the formulation of the method together with the application of the code to an oscillating wing which has the low aspect ratio and low thickness ratio. The correlation work of the computer results with the wind tunnel test data which are obtained at NAL 2 m transonic wind tunnel is also presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000294021","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-30","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":"三菱重工業"},{"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":"Mitsubishi Heavy Industries, Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 満津夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"巽, 重文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishiguro, Mitsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tatsumi, Shigefumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","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":"nalsp0030021.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0030021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36789/files/nalsp0030021.pdf"},"version_id":"1d9e8577-87c2-4f58-988e-3a7967bb4a31"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"振動翼周りの流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常Navier-Stokes方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"Beam-Warming ADI法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"薄翼","subitem_subject_scheme":"Other"},{"subitem_subject":"スレンダ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"格子形成","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"非粘性流","subitem_subject_scheme":"Other"},{"subitem_subject":"差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around oscillating wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Beam Warming ADI method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thin wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"slender wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numeral analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inviscid flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite difference method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamics","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":"遷音速域における振動翼まわりの数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速域における振動翼まわりの数値解析"}]},"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":"36789","relation_version_is_last":true,"title":["遷音速域における振動翼まわりの数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:31:33.985902+00:00"}