{"created":"2023-06-20T15:07:52.437902+00:00","id":37237,"links":{},"metadata":{"_buckets":{"deposit":"58e9707b-d0b1-4c59-a9f2-2b1d2ce958cc"},"_deposit":{"created_by":1,"id":"37237","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37237"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037237","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479781","479779","479778","479777","479780","479776"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effects of compressibility on the stability of three-dimensional boundary layer"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"58","bibliographicPageStart":"57","bibliographicVolumeNumber":"40","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","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":"30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd)","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":"30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"圧縮性3次元境界層の安定性を線形安定性理論に基づいて調べた。境界層分布として一群のFalkner-Skan-Cooke型分布を用いて、マッハ数M(sub e)がそれぞれ0.2と2.0の亜音速および超音速境界層に対して安定性解析を行った。その結果、最大横流れ速度が外部流れ方向速度の5%を越えると、このふたつのマッハ数において横流れ不安定性が支配的になることがわかった。マッハ数に対する最大不安定モードの伝搬角と位相速度の依存性は、横流れ不安定性においては非常に弱いこともわかった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Stability of compressible three dimensional boundary layers is examined on the basis of the linearized stability theory. Stability analysis is made for subsonic and supersonic boundary layers at Mach numbers M(sub e) = 0.2 and 2.0 respectively, using a family of the Falkner-Skan-Cooke type profiles as the boundary layer profiles. The results show that the cross flow instability becomes dominant for both the Mach numbers when the maximum cross flow velocity exceeds 5 percent of the external streamwise velocity. It is also shown that the dependency of the propagation angle and phase speed of the most unstable mode on the Mach number is very weak for the cross flow instability.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001655014","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-40","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":"東京都立科学技術大学 工学部　航空宇宙システム工学科"},{"subitem_text_value":"東京都立科学技術大学 大学院工学研究科"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Department of Aerospace Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan Institute of Technology Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"浅井, 雅人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清野, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 信毅"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asai, Masahito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Seino, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Nobutake","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"3次元境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層不安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"亜音速境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"横流れ不安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"線形安定性理論","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"横流れ速度","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"subsonic boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cross flow instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linearized stability theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cross flow velocity","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":"三次元境界層の安定性に対する圧縮性の影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"三次元境界層の安定性に対する圧縮性の影響"}]},"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":"37237","relation_version_is_last":true,"title":["三次元境界層の安定性に対する圧縮性の影響"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:22:59.691705+00:00"}