{"created":"2023-06-20T15:08:18.577838+00:00","id":37725,"links":{},"metadata":{"_buckets":{"deposit":"cc626511-c1f9-4d6d-9dae-34771e3efe1b"},"_deposit":{"created_by":1,"id":"37725","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37725"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037725","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482686","482687","482689","482688"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Transonic expanding flow through axially symmetric orifices"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"220","bibliographicPageStart":"215","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":"本論文では円断面オリフィスを通る軸対称遷音速気流の特性を見出すための手法について述べる。ホドグラフ法と特性曲線法とを用いて数値解を得た。収縮比、速度プロフィールおよび中心線マッハ数分布を求めた。数値計算結果はShermanによる実験結果と合致することが見られた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes a method of finding the flow pattern of an axially symmetric transonic gas jet through a circular orifice. Numerical solutions were obtained by hodograph transformation and the method of characteristics. The contraction coefficient, velocity profiles and centerline Mach number distributions were calculated. The numerical results are found to agree with the experimental data by Sherman.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168039","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":"東京工業大学 大学院"},{"subitem_text_value":"東京工業大学 大学院"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Institute of Technology Graduate School"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"五十嵐, 弓将"}],"nameIdentifiers":[{"nameIdentifier":"482686","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"三神, 尚"}],"nameIdentifiers":[{"nameIdentifier":"482687","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Igarashi, Yuminobu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482688","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Mikami, Hisashi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482689","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":"nalsp0019039.pdf","filesize":[{"value":"329.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019039.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37725/files/nalsp0019039.pdf"},"version_id":"23cbb87b-1015-439c-aa97-d2c8c27ce2fd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軸対称オリフィス流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称遷音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"自由噴流","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速噴流","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速ガスジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"ホドグラフ法","subitem_subject_scheme":"Other"},{"subitem_subject":"特性曲線法","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"オリフィス収縮係数","subitem_subject_scheme":"Other"},{"subitem_subject":"オリフィス自由流線パターン","subitem_subject_scheme":"Other"},{"subitem_subject":"音速線パターン","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric orifice flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"free jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic gas jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hodograph method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"method of characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orifice contraction coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orifice free stream line pattern","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sonic line pattern","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":"軸対称オリフィスを通る遷音速膨張流","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"軸対称オリフィスを通る遷音速膨張流"}]},"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":"37725","relation_version_is_last":true,"title":["軸対称オリフィスを通る遷音速膨張流"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:13:59.118093+00:00"}