{"created":"2023-06-20T15:07:59.335244+00:00","id":37371,"links":{},"metadata":{"_buckets":{"deposit":"fd4dc9b6-d32e-429d-a3bb-139d12419442"},"_deposit":{"created_by":1,"id":"37371","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37371"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037371","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480401","480404","480406","480403","480405","480400","480402","480407"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル(英)","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulations on high temperature jet impinging normally on the wall"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"360","bibliographicPageStart":"355","bibliographicVolumeNumber":"41","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":"航空宇宙技術研究所 24-26 Jun. 1998 東京 日本","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":"National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"垂直板に入射する高温ジェットは地上からロケットを打ち上げる際に極めて重大な問題になることがある。これまで多くの研究が行われてきた。しかし、流れの機構は充分には明らかにされていない。本研究では垂直板に入射する超音波ジェットについて相互に作用する流れの場の数値計算を行う。ノズル出口と垂直板間の変位を変え、そして相互に作用する流れの場に及ぼす変位の影響を数値的に調査する。計算された流れのパターンと圧力分布は実験との良い一致を示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"High temperature jet impinging on the wall sometimes become quite serious problems in launching the rocket from the ground. Several researches have been conducted by some authors. However, the flow mechanism has not been revealed sufficiently. The interacting flow fields of supersonic jet impinging on the wall are numerically simulated. The displacement between the nozzle exit and the wall is varied and the effects of the displacement on the interacting flow field are investigated numerically. The calculated flow patterns and pressure distributions show good agreements with experiments.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958057","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-41","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":"九州大学 工学部 航空工学科"},{"subitem_text_value":"九州大学 工学部 航空工学科"},{"subitem_text_value":"三菱重工業 長崎研究所"},{"subitem_text_value":"三菱重工業 長崎研究所"}]},"item_5_text_7":{"attribute_name":"著者所属(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagasaki Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagasaki Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"麻生, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大城, 智"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂田, 展康"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"志田, 坦也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oshiro, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shida, Hiroya","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0041057.pdf","filesize":[{"value":"488.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041057.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37371/files/nalsp0041057.pdf"},"version_id":"110cb64b-8d25-4ab7-a2d3-830f8467f7fd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高温ジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"数値計算","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"超音波ジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ場","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"格子","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケット打ち上げ","subitem_subject_scheme":"Other"},{"subitem_subject":"high temperature jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket landing","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":"垂直板に入射する高温ジェットの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"垂直板に入射する高温ジェットの数値シミュレーション"}]},"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":"37371","relation_version_is_last":true,"title":["垂直板に入射する高温ジェットの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:39.325885+00:00"}