{"created":"2023-06-20T15:10:59.560083+00:00","id":40568,"links":{},"metadata":{"_buckets":{"deposit":"11574827-6f97-4f62-9d01-4fbe61b9bf26"},"_deposit":{"created_by":1,"id":"40568","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40568"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040568","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["448726","448727"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Validation of a CFD code for complex configuration"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"28","bibliographicPageStart":"1","bibliographicVolumeNumber":"1376","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"実際の空力設計に適用することを前提として複雑形状の解析を精度よく行えるCFD(計算流体力学)コードの開発を行った。開発したCFDコードの解析結果を風洞実験データと比較し検証することでこのコードの信頼性を確認した。風洞実験による検証作業は2段階で行われ、まず単純な形状であるアロー翼まわりの超音速流で検証を行い次に次世代超音速旅客機を模した翼胴形態まわりの超音速流で検証を行った。これら2つの検証において設計で重要視される揚力、抗力、ピッチングモーメント特性といったグローバルな特性および翼面上のCp分布といったミクロな特性の両方を比較し、実験値と計算値とで良い一致が得られた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The CFD (Computational Fluid Dynamics) code, which is developed to analyze a flow around complex configurations with high resolution, is validated by two kinds of experimental data in order to establish reliability. One is a flow around an arrow wing, which is a simple configuration. Another is a flow around a wing-body configuration, which simulate a next generation supersonic transport. Global properties as lift, drag and pitching moment are compared between experiment and computation, as well as pressure distributions on wing surfaces. These comparisons show good agreement.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001803000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1376","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 計算科学研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Computational Science Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高木, 亮治"}],"nameIdentifiers":[{"nameIdentifier":"448726","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"448727","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001376.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001376.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40568/files/naltr0001376.pdf"},"version_id":"fc17bb93-650b-4607-8b55-93bd5f6204ee"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"複雑形状まわりの流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学コード","subitem_subject_scheme":"Other"},{"subitem_subject":"プログラム検証","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞実験","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"アロー翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼胴形態","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチブロック格子","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速旅客機","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around complex configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"program validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"arrow wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing body configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiblock grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"複雑形状まわりの流れの数値解析手法の検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"複雑形状まわりの流れの数値解析手法の検証"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40568","relation_version_is_last":true,"title":["複雑形状まわりの流れの数値解析手法の検証"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:15:08.418203+00:00"}