{"created":"2023-06-20T15:11:32.250745+00:00","id":41219,"links":{},"metadata":{"_buckets":{"deposit":"966a6be3-cb3a-4fac-898a-d9c3a60a8a73"},"_deposit":{"created_by":1,"id":"41219","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41219"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041219","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451244","451235","451238","451233","451239","451240","451234","451232","451237","451245","451236","451242","451243","451241"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental investigation of static and dynamic ground effect on HOPEALFLEX vehicle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"57","bibliographicPageStart":"1","bibliographicVolumeNumber":"1236","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":"HOPE　ALFLEX(自動着陸実験)実験機開発のための地面効果試験を実施した。本実験の目的は、(1)新しく採用した模型支持システムが一様流に及ぼす影響の予備検証を行うこと。(2)静的地面効果のデータを得ること。(3)動的地面効果のデータを得ること。である。本実験では産業用のロボットを模型支持装置として採用し、ロボットアームの動きをコントロールすることによって、その先端に取り付けられた模型の姿勢、位置を自由に変化させて必要なデータを取ることに成功した。地面効果試験においては、地面板と模型の相対位置を変化させてデータを取る必要があるが、模型の位置と姿勢を自由に変えられるため、効率的な試験ができたばかりでなく、近年注目されている動的な地面効果のデータを取ることも可能となった。動的、静的な地面効果の大きさの比較から、動的効果は高々静的効果程度であるとの結論を得た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A wind tunnel test was conducted to investigate the ground effect on an 8.9 percent model of the ALFLEX (Automatic Landing FLight EXperiment) vehicle. The objectives of this experiment were: (1) To make a preliminary inspection of the influence of the new model supporting system on the main flow; (2) to collect data of the static ground effect; and (3) to collect data of the dynamic ground effect. A robot designed for general industrial use was employed as a tool for model support. The merits of utilizing the robot in our experiment was not only to raise the efficiency of the static measurements but also to make it possible to collect the dynamic data in the ground effect test. Comparison between results from static and dynamic tests showed that the amount of the dynamic ground effect is no more than the static effect.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004249000","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-1236","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 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"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":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大貫, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"季家, 賢一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中安, 英彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"匂坂, 雅一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Onuki, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Rinoie, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakayasu, Hidehiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sagisaka, Masakazu","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":"naltr01236.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01236.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41219/files/naltr01236.pdf"},"version_id":"c4db8702-ea49-4f2f-ad25-ea486518b8d5"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"地面効果","subitem_subject_scheme":"Other"},{"subitem_subject":"動的地面効果試験","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"動的模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボット式模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE小型自動着陸実験機","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":"着陸過程シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン低速空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"慣性力分離","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"ground effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic ground effect test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robot based model support system","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 vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2 rocket assisted orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing process simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane low speed aerodynamic characteristics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inertial force decoupling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support interference","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":"HOPE小型自動着陸実験機8.9％模型の動的・静的地面効果試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPE小型自動着陸実験機8.9％模型の動的・静的地面効果試験"}]},"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":"41219","relation_version_is_last":true,"title":["HOPE小型自動着陸実験機8.9％模型の動的・静的地面効果試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:11:53.657262+00:00"}