{"created":"2023-06-20T15:10:25.234766+00:00","id":40001,"links":{},"metadata":{"_buckets":{"deposit":"d48873d0-bb46-409c-ab52-7cb15f7fe308"},"_deposit":{"created_by":1,"id":"40001","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40001"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040001","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["445949","445946","445948","445947"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Prandtl-Meyer type expansion wave in axi-symmetric supersonic flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"1","bibliographicVolumeNumber":"1332","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"2次元超音速流がプラントル・メイヤー波によって厳密に扱いうるのに対し、軸対称流はこれに対応する有心膨脹波の厳密解が得られていないため、特性曲線法の基礎が充分でないと考えられる。今回線型方程式の相似解によって、3次元有心膨脹波の特性を求め、これとの比較によって特性曲線法の妥当性を検討した。この成果を用いて、軸対称噴流の周期構造を計算し良い結果が得られた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In a two-dimensional flow, an exact analytical form is obtained for Prandtl Meyer waves, so the basis of the characteristic method is well established. But in three dimensional axially symmetric flow, no exact solution exists for such expansion waves. In this report, a new type of similar solution of linearized flow is compared with the result by the characteristic method. This result is used to study the periodic structure of an exhaust jet.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001143000","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 TR-1332","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野溝, 国生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomizo, Kunio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Takashi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001332.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001332.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40001/files/naltr0001332.pdf"},"version_id":"6c0a3c8f-fe46-42c4-a91f-cf2b8d66ecce"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"軸対称超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元流","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称噴流","subitem_subject_scheme":"Other"},{"subitem_subject":"周期構造","subitem_subject_scheme":"Other"},{"subitem_subject":"プラントル・メイヤー波","subitem_subject_scheme":"Other"},{"subitem_subject":"特性曲線法","subitem_subject_scheme":"Other"},{"subitem_subject":"厳密解","subitem_subject_scheme":"Other"},{"subitem_subject":"膨張波","subitem_subject_scheme":"Other"},{"subitem_subject":"線形化流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"相似解","subitem_subject_scheme":"Other"},{"subitem_subject":"線型方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"不足膨張噴流","subitem_subject_scheme":"Other"},{"subitem_subject":"ディフューザ","subitem_subject_scheme":"Other"},{"subitem_subject":"排気プルーム","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"periodic structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Prandtl Meyer wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"characteristics curve method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"exact solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"expansion wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linearized flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"similar solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shortage expansion jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"diffuser","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"exhaust plume","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"軸対称超音速流中のプラントル・メイヤー型膨脹波の解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"軸対称超音速流中のプラントル・メイヤー型膨脹波の解析"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40001","relation_version_is_last":true,"title":["軸対称超音速流中のプラントル・メイヤー型膨脹波の解析"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:17:31.064513+00:00"}