{"created":"2023-06-20T15:08:17.650998+00:00","id":37706,"links":{},"metadata":{"_buckets":{"deposit":"5813a845-a58c-43d3-97fb-d792e2bb27fd"},"_deposit":{"created_by":1,"id":"37706","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37706"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037706","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482595","482597","482594","482596"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Code development for hypersonic real-gas flow simulations toward the design of space vehicles, 2"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"114","bibliographicPageStart":"109","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 10-12 Jun. 1992 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"極超音速流のシミュレーションシステムを開発している。これまでに流れの計算コード、格子形成コードおよび後処理ルーチンとしての平衡化学成分計算コードを開発した。流れの計算コードは、VEG(可変等価ガンマ)を用いた3次元風上流束分割スキームに基づくものを改良して熱伝達分布をシミュレートできるようにした。HOPE(H-2ロケット打上げ型有翼回収機)のまわりの流れ場のシミュレーションを行った。流れの条件はマッハ数15、迎角30度である。熱伝達率の計算結果が得られた。それを実験データと比較し、下面側物体対称線に沿って良い一致をみた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A hypersonic flow simulation system is under development. A flow analysis code, an adaptive grid generation code, and a computation code of equilibrium chemical composition as a post process routine have been developed. The flow analysis code that is based on 3-D upwind flux splitting scheme using the VEG (Variable Equivalent Gamma) method has been improved in order to simulate heat transfer distributions. Numerical simulations are conducted for flow fields around HOPE (H-2 Orbiting Plane). Flow conditions are Mach number of 15 and angle of attack of 30 degrees. Computed heat transfer ratio distributions are obtained. Results are compared with experimental data and good agreement is shown along a body symmetrical line of lower surface.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168020","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-19","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":"三菱重工業"},{"subitem_text_value":"宇宙科学研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中尾, 雅弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 孝藏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakao, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Kozo","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0019020.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019020.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37706/files/nalsp0019020.pdf"},"version_id":"5f7120d7-3a1a-44e3-a908-5cbcaf9a67f2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入物体","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学解析","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":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"解離気体成分分布","subitem_subject_scheme":"Other"},{"subitem_subject":"解適合格子","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamic analysis","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":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dissociated gas component distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solution adaptive grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","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":"空力設計ツールとしての極超音速流計算コードの開発　その2","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"空力設計ツールとしての極超音速流計算コードの開発　その2"}]},"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":"37706","relation_version_is_last":true,"title":["空力設計ツールとしての極超音速流計算コードの開発　その2"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:14:29.266143+00:00"}