{"created":"2023-06-20T15:05:08.109427+00:00","id":34386,"links":{},"metadata":{"_buckets":{"deposit":"961af2c8-e3a2-4426-8bef-37a61f13e6e2"},"_deposit":{"created_by":1,"id":"34386","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"34386"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00034386","sets":["1887:1890","1896:1898:1899:1992"]},"author_link":["419507","419506"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1966-08","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"141","bibliographicPageStart":"117","bibliographicVolumeNumber":"31","bibliographic_titles":[{},{"bibliographic_title":"ISAS report/Institute of Space and Aeronautical Science,University of Tokyo","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A general method of theoretical approach to supersonic flow past lifting bodies of revolution with arbitrary geometry is presented assuming that the flow behind an attached shock wave consists of a basic non-lifting field upon which is superimposed a perturbation field due to small angles of attack and is particularly applied to circularcones as a simple example. It is shown that, although the nonlinearity in fundamental equations predicting the basic field has a predominant effect on aerodynamic characteristics of the body, a linear approximation of perturbation field with respect to angle of attack still seems to be available even if the body is not so slender. Experimental results also confirm this.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA2400529000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Aeronautical Science,University of Tokyo"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0372-1418","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00675986","subitem_source_identifier_type":"NCID"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mechanical Engineering Research Laboratory, Hitachi Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"KARASHIMA, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IWASAKI, Kenjiro","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":"2020-01-24"}],"displaytype":"detail","filename":"SA2400529.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA2400529.pdf","url":"https://jaxa.repo.nii.ac.jp/record/34386/files/SA2400529.pdf"},"version_id":"a461ed68-6fdf-42e4-8c8c-3b5c39cb6cc1"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1992"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"34386","relation_version_is_last":true,"title":["Supersonic Flow Past Pointed Bodies of Revolution at Small Angles of Attack"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:43:04.897667+00:00"}