{"created":"2023-06-20T15:08:25.833007+00:00","id":37878,"links":{},"metadata":{"_buckets":{"deposit":"fbae8e9f-67e2-418f-92b2-e9a4e0990a35"},"_deposit":{"created_by":1,"id":"37878","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37878"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037878","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430739","430740","430738","430741"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Computations of low speed flow about a space-plane"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"284","bibliographicPageStart":"279","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":"遷/超音速流れのシミュレーションに用いた圧縮性ナビエ･ストークス方程式解法コードを低い亜音速の流れにも適用するため、航空宇宙技術研究所の｢数値風洞｣上でスペースプレーンまわりの流れの並列計算機による計算を行った。計算結果はコードが空気力の予測に十分の精度をもつことを示す。したがって、改良によりこのコードを低亜音速から超音速に至る範囲でロバストな流れ計算法とならしめる見込みが得られた。それを実現するには、計算における収束の効率を更に高めることと、流れの詳細なメカニズムを分析することが必要である。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Parallel computation of flow fields around a space-plane has been conducted on the Numerical Wind Tunnel (NWT) at the National Aerospace Laboratory, aiming to apply the compressible Navier-Stokes code which super/transonic flows with to solve low subsonic flow have been simulated fields. Computational results show its sufficient reliability in terms of predicting aerodynamic forces. Thus, a prospect to make the present code a robust flow solver covering from a low subsonic to a supersonic regime with modifications has been obtained. To realize it, further more effort is needed to get convergence efficiency of computation and to analyze the mechanism of microscopic flow phenomena.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004174041","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":"富士通"},{"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":"Fujitsu 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":"松島, 紀佐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","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":"nalsp0027041.pdf","filesize":[{"value":"481.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0027041.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37878/files/nalsp0027041.pdf"},"version_id":"bd2a570f-5354-4dfa-9675-3ac76dfd5e5e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"亜音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDプログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"並列化","subitem_subject_scheme":"Other"},{"subitem_subject":"複合格子法","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD応用","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"数値風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"物体の周りの流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parallelization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multi block domain method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD application","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attack angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around body","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":"スペースプレーンまわりの低マッハ数流れの数値計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スペースプレーンまわりの低マッハ数流れの数値計算"}]},"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":"37878","relation_version_is_last":true,"title":["スペースプレーンまわりの低マッハ数流れの数値計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:47:17.655420+00:00"}