{"created":"2023-06-20T14:39:42.470898+00:00","id":6469,"links":{},"metadata":{"_buckets":{"deposit":"7b3e00ea-808c-4eeb-868c-0c61c2ebe974"},"_deposit":{"created_by":1,"id":"6469","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6469"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006469","sets":["1887:1891","9:789:1067:1073"]},"author_link":["32886","32888","32887","32891","32890","32894","32885","32889","32892","32893"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Prediction of blade forced response by use of a combination of aerodynamic and structural analysis on ITBL network"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"177","bibliographicPageStart":"172","bibliographicVolumeNumber":"JAXA-SP-04-012","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A numerical analysis system has been developed for predicting forced vibration levels of compressor blades of a given blade row subjected to either wakes from an upstream blade row or potential flow disturbances from an upstream/downstream blade row. The system consists of an unsteady aerodynamic analysis and a structural analysis. The unsteady aerodynamic analysis based on an unsteady three-dimensional multi-blade row Reynolds-averaged Navier-Stokes analysis is performed to predict the unsteady aerodynamic load in a multi-blade row environment. The structural analysis using a finite element model is performed to get the mode shape and frequency of the blade. In this paper, the system is established on ITBL (IT-Based Laboratory) network, and applied to a rotor blade of High-Pressure Compressor. As a result, it is found that the pressure perturbation on a rotor blade is to be three-dimensional distribution and vary from blade to blade.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048469029","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-04-012","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":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"宇宙航空研究開発機構"},{"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":"Ishikawajima-Harima Heavy Industries Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"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":"浜辺, 正昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大庭, 芳則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉田, 正廣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 一臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamabe, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oba, Yoshinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Kazuomi","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":"48469029.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48469029.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6469/files/48469029.pdf"},"version_id":"dd05543a-1276-4d94-86d0-c1e4f51883d8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"予測","subitem_subject_scheme":"Other"},{"subitem_subject":"強制振動","subitem_subject_scheme":"Other"},{"subitem_subject":"構造振動","subitem_subject_scheme":"Other"},{"subitem_subject":"タービン翼","subitem_subject_scheme":"Other"},{"subitem_subject":"構造解析","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮機翼","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"後流干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"prediction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"forced vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbine blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressor blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wake interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","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":"ITBL上での空力／構造解析を組み合わせた翼振動応答予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ITBL上での空力／構造解析を組み合わせた翼振動応答予測"}]},"item_type_id":"5","owner":"1","path":["1073","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6469","relation_version_is_last":true,"title":["ITBL上での空力／構造解析を組み合わせた翼振動応答予測"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:55:11.630624+00:00"}