{"created":"2023-06-20T15:07:51.388736+00:00","id":37218,"links":{},"metadata":{"_buckets":{"deposit":"30ce1ea5-b4e6-4928-93fb-cc13dcf344b3"},"_deposit":{"created_by":1,"id":"37218","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37218"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037218","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479702","479707","479698","479704","479708","479709","479700","479705","479706","479703","479711","479701","479699","479710"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"小型自動着陸飛行実験(ALFLEX)のための風洞試験"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"152","bibliographicPageStart":"145","bibliographicVolumeNumber":"39T","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　宇宙開発事業団 28 Feb. 1997 Sydney","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. National Space Development Agency of Japan 28 Feb. 1997 Sydney Australia","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ALFLEX(小型自動着陸飛行実験)の飛翔体開発には、飛翔体の空力特性をできるだけ正確に見積る必要がある。これは搭載する制御システムの設計に不可欠だからである。このため、数種の異なる寸法の飛翔体模型を用いて6回の風洞試験を行い、さらに、開発の最終段階で、サブシステムの性能とその改良結果を確認するために2回の風洞試験を行った。合計8回の風洞試験は、3つの組織において4つの風洞を用いて行われ、この報告では、これら風洞試験結果から推定されるALFLEX飛翔体の空力特性を紹介した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For the development of the ALFLEX (Automatic Landing Flight Experiment) vehicle, it was necessary to estimate its aerodynamic characteristics before as accurately as possible, since they were essential for the design of the control system loaded onboard. To meet this requirement, six wind tunnel tests were conducted using several models of different sizes. In addition, two wind tunnel tests were conducted in the final stage of development to confirm the performance of subsystems or to check the result of the improvement of a subsystem. In this paper, these eight wind tunnel tests made at three organizations employing four wind tunnels are introduced along with the aerodynamic characteristics of the ALFLEX vehicle estimated in those tests.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001565015","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-39T","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"川崎重工業"},{"subitem_text_value":"川崎重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳原, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中安, 英彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"米田, 洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"本田, 直志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"開沼, 史和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福井, 冨久男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagihara, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakayasu, Hidehiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoneda, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Honda, Naoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kainuma, Fumikazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukui, Fukuo","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":"nalsp0039015.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0039015.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37218/files/nalsp0039015.pdf"},"version_id":"643bc91a-2392-498c-942f-a79e417a2bf8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"飛翔体模型支持システム","subitem_subject_scheme":"Other"},{"subitem_subject":"制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"地面効果特性","subitem_subject_scheme":"Other"},{"subitem_subject":"懸吊特性","subitem_subject_scheme":"Other"},{"subitem_subject":"縦特性","subitem_subject_scheme":"Other"},{"subitem_subject":"横特性","subitem_subject_scheme":"Other"},{"subitem_subject":"方向特性","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vehicle model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground effect characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hanging characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"longitudinal characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lateral characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"directional characteristic","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"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Wind tunnel tests for ALFLEX","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Wind tunnel tests for ALFLEX","subitem_title_language":"en"}]},"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":"37218","relation_version_is_last":true,"title":["Wind tunnel tests for ALFLEX"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:16.502901+00:00"}