{"created":"2023-06-20T15:07:28.809696+00:00","id":36850,"links":{},"metadata":{"_buckets":{"deposit":"d551261a-e3a9-4b5c-8db0-823a831f5fac"},"_deposit":{"created_by":1,"id":"36850","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36850"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036850","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477867","477868"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD analysis of HYFLEX aerothermodynamic characteristics"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"110","bibliographicPageStart":"103","bibliographicVolumeNumber":"32","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_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"24-25 Jul. 1996","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":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HYFLEX(極超音速飛行実験)機のCFD(数値流体力学)解析による極超音速熱空力特性評価は、基本設計、詳細設計フェーズにおいて実施され、風洞試験結果とも良好な一致が得られている。今回、改めて HYFLEX 飛行軌道に沿ったCFD計算を行い、熱空力特性についての比較検証を目的として飛行実験データの解析を行った。本解析では、完全気体および再突入時の高温環境下での影響を見積もるための実在気体モデルを使用したナビエ・ストークス方程式を使用し、HYFLEXの空力特性、空力加熱特性について詳細に検討した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Hypersonic CFD (Computational Fluid Dynamics) analysis has been conducted for the evaluation and investigation of HYFLEX (Hypersonic Flight Experiment) aerothermodynamic characteristics. Numerical analysis was also made for the aerodynamic design before HYFLEX flight and favorable agreements with wind tunnel experimental data were obtained. New computations along the HYFLEX flight trajectory starts for the investigation of aerothermodynamic characteristics of reentry flight. In the present analysis, perfect gas and nonequilibrium Navier-Stokes computations are conducted, and aerodynamic characteristics are compared with the flight experiment in detail.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000584012","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-32","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":"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":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","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":"nalsp0032012.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0032012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36850/files/nalsp0032012.pdf"},"version_id":"1289ca75-a3bc-4788-9925-2c87a7059950"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱特性","subitem_subject_scheme":"Other"},{"subitem_subject":"熱空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学解析","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達分布","subitem_subject_scheme":"Other"},{"subitem_subject":"断面等圧線","subitem_subject_scheme":"Other"},{"subitem_subject":"オイルフロー","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerothermodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure contour","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oil flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbiting plane","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 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