{"created":"2023-06-20T15:07:51.524299+00:00","id":37220,"links":{},"metadata":{"_buckets":{"deposit":"fbcc20f2-7a2c-4df8-b5a4-63367167f0cb"},"_deposit":{"created_by":1,"id":"37220","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37220"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037220","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479718","479721","479719","479720"],"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)の飛行試験から得た地面効果"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"172","bibliographicPageStart":"165","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)の飛行実験は、オーストラリア南部のウーメラにおいて行われ、1996年7月6日から13回の着陸試験を行った。すべての模型飛翔体の着陸性能は、地面に強く影響された。この報告では、無人・無推力飛翔体の飛行実験データに基づいて地面効果を解析する方法を述べ、ALFLEX飛翔体の地面効果特性を示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The ALFLEX (Automatic Landing Flight Experiment) flight experiment was carried out in Woomera in South Australia, and 13 landing trials beginning on July 6, 1996, were conducted. The landing performance of all flying vehicles is strongly influenced by the ground. This paper describes a ground effect analysis method based on the flight experiment data of unmanned nonthrust vehicle, and gives ground effect characteristics of the ALFLEX.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001565017","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":"宇宙開発事業団"}]},"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 Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"岡田, 典秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"水藤, 貴靖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okada, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suito, Takanobu","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":"nalsp0039017.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0039017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37220/files/nalsp0039017.pdf"},"version_id":"ba3d0437-4226-4f51-8d06-7b540c4c9dcb"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"地面効果","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸試験","subitem_subject_scheme":"Other"},{"subitem_subject":"無人無推力飛翔体","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸性能","subitem_subject_scheme":"Other"},{"subitem_subject":"進入法","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸進入","subitem_subject_scheme":"Other"},{"subitem_subject":"降下率","subitem_subject_scheme":"Other"},{"subitem_subject":"対空速度","subitem_subject_scheme":"Other"},{"subitem_subject":"迎え角","subitem_subject_scheme":"Other"},{"subitem_subject":"操縦舵面","subitem_subject_scheme":"Other"},{"subitem_subject":"縦揺れ率","subitem_subject_scheme":"Other"},{"subitem_subject":"高度誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"滑走路傾斜","subitem_subject_scheme":"Other"},{"subitem_subject":"束縛渦","subitem_subject_scheme":"Other"},{"subitem_subject":"ground effect","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":"unmanned nonthrust vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"approach method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing approach","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sink rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airspeed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control surface","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitch rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"altitude error","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"runway slope","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bound vortex","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":"Ground effects obtained from flight tests of ALFLEX","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Ground effects obtained from flight tests of 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":"37220","relation_version_is_last":true,"title":["Ground effects obtained from flight tests of ALFLEX"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:14.409597+00:00"}