{"created":"2023-06-20T16:37:32.440960+00:00","id":7314,"links":{},"metadata":{"_buckets":{"deposit":"6e377fb4-8e48-4782-b2e5-2500d6ab03fe"},"_deposit":{"created_by":3,"id":"7314","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"7314"},"status":"published"},"_oai":{"id":"oai:kindai.repo.nii.ac.jp:00007314","sets":["14:923:1711:1721","21:3039:3241:3285"]},"author_link":["12518","12519","12520"],"item_2_alternative_title_3":{"attribute_name":"その他（別言語等）のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"<Original Papers>Study on Boundary Layer Control of Supersonic Jet Flow Issued from Divergent Nozzle: 1st Report, In fluence of Stagnation Pressure of Main Jet Flow"}]},"item_2_biblio_info_21":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-12-01","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"44","bibliographicPageEnd":"102","bibliographicPageStart":"93","bibliographic_titles":[{"bibliographic_title":"近畿大学工学部研究報告"},{"bibliographic_title":"Research reports of the Faculty of Engineering, Kinki University","bibliographic_titleLang":"en"}]}]},"item_2_description_33":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"[synopsis]In this paper, it aimed to clarify the behavior and the flow field of a supersonic jet flow issuing from a divergent nozzle widely used in industry. Especially, the separation point of the flow was controlled by vertical control jets to the separated supersonic jet flow at the divergent part of the nozzle. By such a method, the boundary layer control of the supersonic jet flow issuing from the divergent nozzle was clarified. In this time, the flow field of the main jet flow has been clarified when the control jets were issued for the main jet flow with various stagnation pressures. Experiments and numerical analyses were completed when the stagnation pressure ratios of the main jet flow were given as Po/Pa ＝ 1.0, 3.0, 6.0 and the stagnation pressure ratio of the control jets were given as Pc/Pa ＝ 3.0. The control jets were vertically issued from eight small holes for the main jet flow. Moreover, numerical analyses were also made when the stagnation pressure ratios of the main jet flow were given as Po/Pa ＝ 10.0 and 20.0. In the experiment, the total pressures were measured around the exit of the divergent nozzle and the equi-total pressure distributions were examined. In the numerical analysis, the velocity contours of the flow were examined for the inside of the divergent nozzle and the downstream region of the flow. As a result, the main jet flow issuing from the divergent nozzle didn't be a round jet by a remarkable influence from the control jets. Moreover, it was found that the shape of the main jet flow was influenced considerably by difference of the stagnation pressure ratio.","subitem_description_type":"Abstract"}]},"item_2_description_41":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_description":"application/pdf","subitem_description_type":"Other"}]},"item_2_publisher_14":{"attribute_name":"出版者 名前","attribute_value_mlt":[{"subitem_publisher":"近畿大学工学部"}]},"item_2_source_id_22":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0386491X","subitem_source_identifier_type":"ISSN"}]},"item_2_text_7":{"attribute_name":"著者(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"YANG, Nianru"},{"subitem_text_language":"en","subitem_text_value":"TAKEICHI, Yasutomo"},{"subitem_text_language":"en","subitem_text_value":"KOJIMA, Tadatomo"}]},"item_2_text_8":{"attribute_name":"著者 所属","attribute_value_mlt":[{"subitem_text_value":"近畿大学; 研究員"},{"subitem_text_value":"近畿大学大学院システム工学研究科"},{"subitem_text_value":"近畿大学工学部知能機械工学科"}]},"item_2_text_9":{"attribute_name":"著者所属(翻訳)","attribute_value_mlt":[{"subitem_text_value":"Researcher, Kinki University"},{"subitem_text_value":"Graduate School of Systems Engineering, Kinki University"},{"subitem_text_value":"Department of Intelligent Mechanical Engineering, Faculty of Engineering, Kinki University"}]},"item_2_version_type_12":{"attribute_name":"版","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"楊,  念儒"},{"creatorName":"&EMPTY&","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"武市,  恭和"},{"creatorName":"タケチ, ヤストモ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"児島,  忠倫"},{"creatorName":"コジマ, タダトモ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-02-18"}],"displaytype":"detail","filename":"AN00063799-20101220-0093.pdf","filesize":[{"value":"5.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AN00063799-20101220-0093.pdf","url":"https://kindai.repo.nii.ac.jp/record/7314/files/AN00063799-20101220-0093.pdf"},"version_id":"2455a3f0-b4c2-477f-9a06-78cafd7c782c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Supersonic Flow","subitem_subject_scheme":"Other"},{"subitem_subject":"Compressible Flow","subitem_subject_scheme":"Other"},{"subitem_subject":"Boundary Layer","subitem_subject_scheme":"Other"},{"subitem_subject":"Turbulent Flow","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock Wave","subitem_subject_scheme":"Other"},{"subitem_subject":"Divergent Nozzle","subitem_subject_scheme":"Other"},{"subitem_subject":"Separation","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"<研究論文>広がりノズルから噴出される超音速噴流の境界層制御に関する研究--第1報主噴流のよどみ圧力の影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<研究論文>広がりノズルから噴出される超音速噴流の境界層制御に関する研究--第1報主噴流のよどみ圧力の影響"}]},"item_type_id":"2","owner":"3","path":["1721","3285"],"pubdate":{"attribute_name":"公開日","attribute_value":"2011-02-21"},"publish_date":"2011-02-21","publish_status":"0","recid":"7314","relation_version_is_last":true,"title":["<研究論文>広がりノズルから噴出される超音速噴流の境界層制御に関する研究--第1報主噴流のよどみ圧力の影響"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-06-21T00:18:49.197403+00:00"}