{"created":"2023-06-20T15:11:30.877083+00:00","id":41190,"links":{},"metadata":{"_buckets":{"deposit":"6a72c9e3-c5b0-4e51-bb4a-fee053dbb160"},"_deposit":{"created_by":1,"id":"41190","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41190"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041190","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451066","451062","451061","451064","451067","451060","451065","451063"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Investigation of experimental bent-nose biconic design in supersonic flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"1","bibliographicVolumeNumber":"1205","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":"AOTV(空力制動型軌道間輸送機)の1形態である屈曲2重円錐の超音速風洞実験結果を示す。超高速飛行体についても低超音速域空力性能試験の必要が考えられる。本試験は特に大迎角試験、表面の流れの剥離測定、底面圧計測および簡単な理論推定法のチェックなどに重点がおかれた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Preliminary wind tunnel tests of a Bent-Nose Biconic were conducted in the NAL 1m X 1m blow-down supersonic wind tunnel to evaluate its aerodynamics in the moderate supersonic range. Aerodynamic data at attack angles of up to 50 deg was obtained for a 30 deg bent-sting. A flow-separated zone on the rear side of the body was observed by surface pressure distribution and oil-flow tests. Estimates based on Newtonian flow theory were not accurate when the attack angle was small for this rather slender configuration.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004220000","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-1205","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 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"},{"subitem_text_value":"東京農工大学 工学部　機械システム工学科"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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"},{"subitem_text_language":"en","subitem_text_value":"Tokyo University of Agriculture and Technology Department of Mechanical Systems Engineering, Faculty of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Kiyomichi","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":"naltr01205.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01205.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41190/files/naltr01205.pdf"},"version_id":"a2cacc0f-87fa-4fa9-a3af-bd89f0e5802f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"鼻曲り2重円錐","subitem_subject_scheme":"Other"},{"subitem_subject":"AOTV","subitem_subject_scheme":"Other"},{"subitem_subject":"空力制動型軌道間輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙飛行体","subitem_subject_scheme":"Other"},{"subitem_subject":"大迎角試験","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布計測","subitem_subject_scheme":"Other"},{"subitem_subject":"オイルフロー試験","subitem_subject_scheme":"Other"},{"subitem_subject":"底面圧計測","subitem_subject_scheme":"Other"},{"subitem_subject":"凹面底面圧","subitem_subject_scheme":"Other"},{"subitem_subject":"平面底面圧","subitem_subject_scheme":"Other"},{"subitem_subject":"ニュートン流近似","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bent nose biconic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AOTV","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aeroassisted Orbital Transfer Vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large angle of attack test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oil flow test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"base pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"concave base base pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flat base base pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Newtonian flow approximation","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":"屈曲2重円錐の超音速風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"屈曲2重円錐の超音速風洞試験"}]},"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":"41190","relation_version_is_last":true,"title":["屈曲2重円錐の超音速風洞試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:23.529655+00:00"}