{"created":"2023-06-20T15:08:16.881987+00:00","id":37690,"links":{},"metadata":{"_buckets":{"deposit":"5690ec56-d0a2-41ae-89f7-4cf8fddbda1e"},"_deposit":{"created_by":1,"id":"37690","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37690"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037690","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482518","482515","482516","482519","482517","482520"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Rarefied gas numerical wind tunnel. 8:HOPE"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"17","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":"飛行物体3次元全機形状のまわりの希薄気体流れのシミュレーションを目的として開発された「希薄気体数値風洞」をH-2ロケット打上げ型有翼回収機(HOPE)の場合に適用した。流れ場の様子や空力特性についての結果を示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The 'Rarefied Gas Numerical Wind Tunnel (RGNWT)' developed for the simulation of rarefied gas flows around three dimensional whole flight bodies is applied to the H-2 Orbiting Plane (HOPE). Some flowfield properties and aerodynamic characteristics are presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168004","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":"航空宇宙技術研究所"},{"subitem_text_value":"大興電子通信"},{"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"},{"subitem_text_language":"en","subitem_text_value":"Daiko Denshi Tsushin 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":"古浦, 勝久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高平, 幹成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松本, 裕昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koura, Katsuhisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahira, Mikinari","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumoto, Hiroaki","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":"nalsp0019004.pdf","filesize":[{"value":"343.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37690/files/nalsp0019004.pdf"},"version_id":"67ace6b4-87e2-49af-909d-a77c2e5a47a0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"直接シミュレーションモンテカルロ法","subitem_subject_scheme":"Other"},{"subitem_subject":"希薄気体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"自由分子流","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達特性","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波干渉空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"クヌーセン数","subitem_subject_scheme":"Other"},{"subitem_subject":"分子分布","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"数値風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"分子衝突モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"可変軟球分子モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"direct simulation Monte Carlo method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rarefied gas dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free molecular flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock interaction aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Knudsen number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"molecular distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"molecular collision modelling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"variable soft sphere molecular model","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 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