{"created":"2023-06-20T15:07:30.291969+00:00","id":36872,"links":{},"metadata":{"_buckets":{"deposit":"cbfd937c-c73e-4c6a-83dc-c17ff6c9e65e"},"_deposit":{"created_by":1,"id":"36872","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36872"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036872","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477944","477948","477946","477943","477947","477945"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Validation of the computation of hypersonic flow with real gas effects"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"72","bibliographicPageStart":"67","bibliographicVolumeNumber":"34","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":"航空宇宙技術研究所 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"化学平衡であると推定される実在気体効果をともなう極超音速流の数値解析を、HEG(ゲッチンゲン高エンタルピー風洞)衝撃風洞試験データとの比較により検証した。流れ解析システムはマルチブロック型構造格子を用い、化学平衡実在気体効果の評価のための曲線あてはめ法による有限体積TVD(Total Variation Diminishing)風上スキームに基づいている。球まわりと単純翼胴模型まわりのそれぞれの流れを計算した。球まわりの流れの数値結果は、よどみ点における熱流束を考えると衝撃風洞試験データと非常によく一致した。単純翼胴模型の結果は衝撃波・衝撃波干渉による位置と熱流束ピーク値に関する実在気体効果を考慮することによって、凍結流の結果と比較して定性的に向上した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The validation of the computation of hypersonic flow with real gas effects, that is assumed to be chemical equilibrium, have been carried out by the comparison with the HEG (High Enthalpy shock tunnel in Goettingen) shock tunnel test data. The flow analysis system uses a structured multi-block grid, and is based on finite volume TVD (Total Variation Diminishing) upwind scheme with the curve fitting to estimate chemical equilibrium real gas effects. Calculations were done to the flows around a sphere and the simple wing-body model respectively. The numerical results of the flow around a sphere showed very good agreement with the shock tunnel test data in the view of heat flux at a stagnation point. The results of the simple wing-body model were qualitatively improved by taking account of real gas effects with respect to the location and value of peak heat flux by shock-shock interaction, compared with frozen flow results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685013","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-34","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":"川崎重工業 航空宇宙事業本部"},{"subitem_text_value":"川崎重工業 航空宇宙事業本部"},{"subitem_text_value":"宇宙開発事業団"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Space Project Engineering Department"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd Space Project Engineering Department"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岸本, 琢司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"花光, 明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"尾藤, 日出夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kishimoto, Takuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanamitsu, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Bito, Hideo","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":"nalsp0034013.pdf","filesize":[{"value":"621.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36872/files/nalsp0034013.pdf"},"version_id":"8cc59172-40b4-49b3-b193-3d9f41e9dc91"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"化学平衡","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ解析システム","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチブロック格子","subitem_subject_scheme":"Other"},{"subitem_subject":"翼胴模型","subitem_subject_scheme":"Other"},{"subitem_subject":"有限体積法","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD風上スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"凍結流","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス解析システム","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical equilibrium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow analysis system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multi block grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing body model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite volume method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD upwind scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"frozen flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes analysis system","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":"実在気体効果をともなう極超音速流解析の検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"実在気体効果をともなう極超音速流解析の検証"}]},"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":"36872","relation_version_is_last":true,"title":["実在気体効果をともなう極超音速流解析の検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:09.957030+00:00"}