{"created":"2023-06-20T15:13:56.788882+00:00","id":43914,"links":{},"metadata":{"_buckets":{"deposit":"b6d1395f-1d76-4dad-8581-e622223f0912"},"_deposit":{"created_by":1,"id":"43914","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43914"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043914","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466320","466319"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Pressure Coefficient of Supersonic Flows Over Cone-Cylinder"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"6","bibliographicVolumeNumber":"331","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical calculation of supersonic flows of a perfect gas over a cone-cylinder is treated.Characteristic method is applied and this method found useful for a cone-cylinder with slope discontinuities.In this report,the nonlinear effect is investigated and compared with the linearized theory.This calculation is treated from Mach 1.5 to 6.0","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0331000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TM-331","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所宇宙研究グループ"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野溝, 国生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOMIZO, Kunio","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00331.pdf","filesize":[{"value":"299.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00331.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43914/files/naltm00331.pdf"},"version_id":"2a09d8bc-4437-4164-95e5-9006471934c0"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"超音速に於ける円錐・円筒物体上の圧力係数","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速に於ける円錐・円筒物体上の圧力係数"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43914","relation_version_is_last":true,"title":["超音速に於ける円錐・円筒物体上の圧力係数"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:05:42.006765+00:00"}