{"created":"2023-06-20T15:10:44.467503+00:00","id":40314,"links":{},"metadata":{"_buckets":{"deposit":"bfe6a8e3-7dea-4c31-8c52-5edd0e0f29e5"},"_deposit":{"created_by":1,"id":"40314","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40314"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040314","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["447303","447304","447300","447296","447298","447294","447292","447301","447297","447295","447299","447293","447305","447302"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Two parallel streams model for drag reduction of separated booster"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"16","bibliographicPageStart":"1","bibliographicVolumeNumber":"1367","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":"物体後流のように速度一様でない超音速流中に置かれた物体の抵抗減少の問題は、切り離された下段ロケットによる上段ロケットへの追突を考えるとき重要な要素となるものである。このような場合の超音速後流のモデルとして最も簡単な2平行流を考え、その中の衝撃波伝播を扱うことによって航技研に於けるロケット段間分離実験結果を説明できることが示される。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For example in wake flow, remarkable drag reduction occurs nonuniform supersonic flow. This phenomenon is important to avoid collision from behind by separated booster. The most simple model for such flow is a set of two parallel flows with different velocities. Analysis for shock wave transfer between these streams gives a reasonable explanation for the results of experiments in NAL.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001674000","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-1367","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 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"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 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"}]},"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 Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野溝, 国生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"近藤, 洋史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"馬場, 滋夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomizo, Kunio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Kiyomichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kondo, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Baba, Shigeo","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":"naltr0001367.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001367.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40314/files/naltr0001367.pdf"},"version_id":"3b7ef075-9e8d-4f0a-ad46-23360ddbec3b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"多段ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットブースタ分離","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速後流","subitem_subject_scheme":"Other"},{"subitem_subject":"2平行流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波伝搬","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力低減","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速平行流","subitem_subject_scheme":"Other"},{"subitem_subject":"空気抵抗低減","subitem_subject_scheme":"Other"},{"subitem_subject":"multistage rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"roket booster separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wake flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two parallel flow model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave propagation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic parallel flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air resistance reduction","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 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