{"created":"2023-06-20T15:08:02.241244+00:00","id":37429,"links":{},"metadata":{"_buckets":{"deposit":"2f996e3a-30ab-4b0e-8e09-c24c9fd8e66d"},"_deposit":{"created_by":1,"id":"37429","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37429"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037429","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480730","480731","480728","480729"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flow instability due to shock-boundary layer interaction in region with narrow clearance"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"112","bibliographicPageStart":"109","bibliographicVolumeNumber":"43","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publicationa 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 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) 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 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"共軸環状ノズルを流れる非定常流れ場を数値計算した。正確なデータを得るために、計算は高次精度の数値計算コードを用いて行った。狭い隙間は超音波ノズルの形をしており、衝撃波が境界層との干渉の結果発生する。このために連続的に振動する流れが生成される。この現象はある種の擬似衝撃波不安定性と考えることができる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The unsteady flow field in a coaxial annular nozzle is numerically calculated. To obtain accurate data, calculation is performed by using a high-order accuracy numerical code. The narrow clearance takes a shape of supersonic nozzle, where shock waves are formed as a result of interacting with the boundary layer. This causes the flow to oscillate continuously. This phenomenon is considered to be a kind of pseudo-shock instability.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001960032","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-43","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":"名古屋大学 大学院工学研究科"},{"subitem_text_value":"名古屋大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"古川, 拓"}],"nameIdentifiers":[{"nameIdentifier":"480728","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 佳朗"}],"nameIdentifiers":[{"nameIdentifier":"480729","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Furukawa, Taku","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480730","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480731","nameIdentifierScheme":"WEKO"}]}]},"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":"nalsp0043032.pdf","filesize":[{"value":"779.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0043032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37429/files/nalsp0043032.pdf"},"version_id":"03a95427-5dce-4d4b-ab55-64c17e975fdc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"有限体積法","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"共軸2重円筒","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波-境界層干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波振動","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常ノズル流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"擬似衝撃波不安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite volume method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coaxial annular duct","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave boundary layer interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady nozzle flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pseudo shock instability","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":"狭い隙間内における衝撃波と境界層の干渉による不安定流れ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"狭い隙間内における衝撃波と境界層の干渉による不安定流れ"}]},"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":"37429","relation_version_is_last":true,"title":["狭い隙間内における衝撃波と境界層の干渉による不安定流れ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:19:04.212444+00:00"}