{"created":"2023-06-20T15:13:31.973857+00:00","id":43452,"links":{},"metadata":{"_buckets":{"deposit":"a584e053-936b-4fc5-9ca9-fec33888f9b4"},"_deposit":{"created_by":1,"id":"43452","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43452"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043452","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463720","463719","463718","463717","463722","463721"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The Role of Computational Fluid Dynamics in Aeronautical Engineering (8) -A Mixed Compression Inlet for a Supersonic Airplane-"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"126","bibliographicPageStart":"121","bibliographicVolumeNumber":"14","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 SP-14","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A numerical investigation on a supersonic mixed-compression inlet is carried out. The inlet is designed for Mach 2.5 by applying the Method of Characteristics. Realistic ramp bleed and throat bypass systems are simulated by a two-dimensional, finite volume, multi-block TVD Navier-Stokes code. From the calculations, the role of ramp bleed and throat bypass systems are revealed. And the mechanism of improving the pressure recovery ahead of an inlet \"unstart\" is found for the first time in detail. The results also show that the throat gap, or slot, constructs an optimum equivalent wall configuration automatically by the flow conditions around the systems. This noteworthy result can be obtained because of the great advantage of the CFD approach.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0014019","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 SP-14","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":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"川崎重工業株式会社岐阜技術研究所"},{"subitem_text_value":"川崎重工業株式会社ジェットエンジン事業部"},{"subitem_text_value":"東北大学流体科学研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Gifu Technical Institute Kawasaki Heavy Industries, Ltd."},{"subitem_text_language":"en","subitem_text_value":"Jet Engine Division Kawasaki Heavy Industries, Ltd."},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science Tohoku University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤本, 朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"丹羽, 伸夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沢田, 恵介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujimoto, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Niwa, Nobuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawada, Keisuke","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":"nalsp0014019.pdf","filesize":[{"value":"475.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0014019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43452/files/nalsp0014019.pdf"},"version_id":"1f415748-67b2-4230-ace4-5fff95e30472"}]},"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":"設計における数値解析の活用について(その8): 超音速機用混合圧縮インテーク","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"設計における数値解析の活用について(その8): 超音速機用混合圧縮インテーク"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43452","relation_version_is_last":true,"title":["設計における数値解析の活用について(その8): 超音速機用混合圧縮インテーク"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:14:28.290486+00:00"}