{"created":"2023-06-20T14:36:16.490639+00:00","id":2587,"links":{},"metadata":{"_buckets":{"deposit":"51391aae-24e8-4cfb-aa2d-04571096ebbf"},"_deposit":{"created_by":1,"id":"2587","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2587"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002587","sets":["1887:1893","9:1090:1230:1240"]},"author_link":["7530","7534","7527","7535","7533","7536","7529","7537","7526","7524","7525","7528","7523","7532","7531","7538"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Force tests of an AGARD calibration model B in the JAXA 0.5 m hypersonic wind tunnel at nominal Mach numbers of 5 and 7"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-07-31","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RM-09-001","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙航空研究開発機構(JAXA)風洞技術開発センターは0.5m極超音速風洞(HWT1)、1.27m極超音速風洞(HWT2)及び0.44m極超音速衝撃風洞(HST)の3つの極超音速風洞を擁している。HWT1では出口直径が0.5mのノズルを交換することによりマッハ数5，7，9の試験が可能である。本稿ではAGARD-B標準模型を用いた6分力試験をHWT1においてマッハ数5及び7で行い、空力特性データを取得したのでその結果を報告する。AGARD-B標準模型は超音速、極超音速領域をカバーする有翼形状の標準模型のひとつであり、国内外の多くの風洞で試験が行われている。マッハ数5の試験結果を他の風洞試験結果と比較し、よく一致することが分かった。他風洞で得られた異なるマッハ数でのデータとの比較においても連続性が認められ、信頼性のある試験結果を得ることができた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Wind Tunnel Technology Center (WINTEC) has three hypersonic wind tunnels: the 0.5 m Hypersonic Wind Tunnel (HWT1), the 1.27 m Hypersonic Wind Tunnel (HWT2) and the 0.44 m Hypersonic Shock Tunnel (HST) at the Japan Aerospace Exploration Agency (JAXA). The HWT1 has three interchangeable nozzles with an exit diameter of 0.5 m for Machnumbers of 5, 7 and 9. Force tests were carried out using an AGARD-B calibration model in the HWT1 at nominal Mach numbers of 5 and 7. AGARD-B models have been used as one of the winged calibration models in supersonic and hypersonic wind tunnels. In this report, aerodynamic characteristics of the AGARD-B calibration model at low angles of attack are discussed in Mach 5 and 7 hypersonic flows. Experimental results of Mach 5 showed good agreement with those of other wind tunnels. The data obtained among the HWT1 and other tunnels were correlated well with the free stream Mach number.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064378000","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: JAXA-RM-09-001","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","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":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター"},{"subitem_text_value":"LBM流体力学研究所"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター"},{"subitem_text_value":"航空宇宙技術振興財団"},{"subitem_text_value":"航空宇宙技術振興財団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"LBM Computational Fluid Dynamics Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aero-Space Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aero-Space Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"津田, 尚一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小山, 忠勇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平林, 則明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡利, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤井, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 晃祥"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木伏, 淳子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuda, Shoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koyama, Tadao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirabayashi, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watari, Minoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujii, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Akiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kibushi, Junko","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":"2020-01-15"}],"displaytype":"detail","filename":"64378000.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64378000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2587/files/64378000.pdf"},"version_id":"000b91d6-66f4-4d41-b1f4-3e3f3d9608f3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Force tests, Hypersonic wind tunnel, AGARD calibration model B","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":"0.5m極超音速風洞におけるマッハ5及び7 AGARD-B標準模型試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"0.5m極超音速風洞におけるマッハ5及び7 AGARD-B標準模型試験"}]},"item_type_id":"3","owner":"1","path":["1240","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2587","relation_version_is_last":true,"title":["0.5m極超音速風洞におけるマッハ5及び7 AGARD-B標準模型試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:19:32.859484+00:00"}