{"created":"2023-06-20T14:39:00.165267+00:00","id":5666,"links":{},"metadata":{"_buckets":{"deposit":"f410f2e8-6c23-475c-9505-d8ab77cfc349"},"_deposit":{"created_by":1,"id":"5666","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5666"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005666","sets":["1887:1891","9:789:972:991"]},"author_link":["27776","27777"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"120","bibliographicPageStart":"112","bibliographicVolumeNumber":"JAXA-SP-07-008E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Unsteady aerodynamics of two dimensional supercritical wing profile in transonic regime was investigated by Navier-Stokes code. First harmonic components of the unsteady aerodynamics obtained by simulation for forced oscillations of heaving and pitching mode were plotted to the amplitude of oscillations and it shows nonlinearity of the unsteady aerodynamics in small amplitude region. Stability analysis based on the first harmonic components of the unsteady aerodynamics also shows nonlinear trend. Limit Cycle Oscillation (LCO) of small amplitude about 0.1 deg could exist from the stability analysis and simulation was carried out, Nolinearity of unsteady aerodynamics in small amplitude range is affected by transition point, which interferes with unsteady pressure distribution in local supersonic region on upper surface. These computational results are described in this paper.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063824011","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: JAXA-SP-07-008E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齊藤, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Kenichi","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":"2020-01-16"}],"displaytype":"detail","filename":"63824011.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63824011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5666/files/63824011.pdf"},"version_id":"d18aceb1-1099-4d9c-931c-449afaf562f2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"非定常空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"粘性流","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"強制振動","subitem_subject_scheme":"Other"},{"subitem_subject":"翼プロフィル","subitem_subject_scheme":"Other"},{"subitem_subject":"リミットサイクル振動","subitem_subject_scheme":"Other"},{"subitem_subject":"非線形性","subitem_subject_scheme":"Other"},{"subitem_subject":"超臨界翼","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"viscous flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"forced vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing profile","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"limit cycle oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonlinearity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supercritical wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier-Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Nonlinearity of the unsteady aerodynamics of the viscous flow on supercritical wing in transonic regime","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Nonlinearity of the unsteady aerodynamics of the viscous flow on supercritical wing in transonic regime","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["991","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5666","relation_version_is_last":true,"title":["Nonlinearity of the unsteady aerodynamics of the viscous flow on supercritical wing in transonic regime"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:09:43.900418+00:00"}