{"created":"2023-06-20T15:08:25.977374+00:00","id":37881,"links":{},"metadata":{"_buckets":{"deposit":"0c38101c-132b-49ad-9809-26f6344c28b0"},"_deposit":{"created_by":1,"id":"37881","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37881"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037881","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430751","430750","430748","430749"],"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 unsteady viscous flow around an airfoil with oscillating spoiler"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"302","bibliographicPageStart":"297","bibliographicVolumeNumber":"27","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"圧縮性ナビエ･ストークス方程式を用いて、振動するスポイラをもつ翼型のまわりの非定常粘性流れの数値シミュレーションを行った。Yee-HartenのTVDスキームおよびBaldwin-Lomaxの代数的乱流モデルを利用した。低亜音速および遷音速マッハ数における振動スポイラ付き16%翼厚スーパークリティカル翼型上の非定常圧力分布を計算し、既存の実験データと比較した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical simulations of unsteady viscous flows around an airfoil with oscillating spoiler have been performed using the compressible Navier-Stokes equations. The Yee-Harten Total Variation Diminishing (TVD) scheme and the Baldwin-Lomax algebraic turbulence model are employed. The unsteady pressure distributions on the 16 percent thick supercritical airfoil with oscillating spoiler in low subsonic and transonic Mach numbers have been calculated, being compared with the existing experimental data.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004174044","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-27","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":"九州大学 工学部 航空工学科"},{"subitem_text_value":"航空宇宙技術研究所 数理解析部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Computational Sciences Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"磯貝, 紘二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 正廣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Isogai, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Masahiro","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0027044.pdf","filesize":[{"value":"347.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0027044.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37881/files/nalsp0027044.pdf"},"version_id":"b1513795-0713-43ca-9c8b-b155e2a02aa7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"振動スポイラ","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常粘性流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常剥離流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"スーパークリティカル翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"TVDスキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"低亜音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"oscillating spoiler","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady viscous flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady separated flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Compressible Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supercritical airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low subsonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady flow","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":"振動するスポイラを持つ2次元翼まわりの流れの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"振動するスポイラを持つ2次元翼まわりの流れの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":"37881","relation_version_is_last":true,"title":["振動するスポイラを持つ2次元翼まわりの流れの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:47:12.237407+00:00"}