{"created":"2023-06-20T15:07:49.234360+00:00","id":37182,"links":{},"metadata":{"_buckets":{"deposit":"bd00c1ab-5468-4edd-a38b-a064328b6c10"},"_deposit":{"created_by":1,"id":"37182","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37182"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037182","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479359","479358"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Proceedings both of the 58th and 59th Wind Tunnel Research Conferences"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"232","bibliographicPageStart":"1","bibliographicVolumeNumber":"38","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","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":"22-23 May 1997 (58th). 27-28 Nov. 1997 (59th)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文集では、以下の風洞研究について論じた。大型高温衝撃風洞(HIEST)の設計と空力試験、超音速風洞および遷音速風洞のデータ処理設備、2次元風洞の改修、アーク加熱気流の計測、高仰角試験、感圧塗料のサンプル特性試験、低速および遷音速風洞試験、ALFLEX(小型自動着陸実験)実験機空力データベース、飛行速度ベクトル計測システムの特性と装置、高速多点圧力計測装置、風洞計測システム、およびHOPE(H-2ロケット打上げ型有翼回収機)におけるピッチングモードフラッタ。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The following researches on wind tunnel are discussed: design and aerodynamic tests of High Enthalpy Shock Tunnel (HIEST), data processing equipment of both supersonic and transonic wind tunnels, improvement of two-dimensional wind tunnel, measurements of an arc heated flow, high angle of attack test, sample tests of pressure-sensitive paints, wind tunnel test of both low-speed and transonic flows, ALFLEX aerodynamic database, characteristic and equipment of air data system, high-speed pressure acquisition system, wind tunnel instrumentation system, and pitching mode flutter for HOPE (H-2 Orbiting Plane).","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434000","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-38","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":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"航空宇宙技術研究所"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"National Aerospace Laboratory","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HIEST","subitem_subject_scheme":"Other"},{"subitem_subject":"大型高温衝撃風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"空力試験","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"高仰角試験","subitem_subject_scheme":"Other"},{"subitem_subject":"感圧塗料","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞計測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"感温塗料","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行速度ベクトル計測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"HIEST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy shock tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high angle attack test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure sensitive paint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tunnel instrumentation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature sensitive paint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air data system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","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 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