{"created":"2023-06-20T15:10:04.529449+00:00","id":39669,"links":{},"metadata":{"_buckets":{"deposit":"5ac16d7d-c0bf-4876-aaa2-64864aa644e6"},"_deposit":{"created_by":1,"id":"39669","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39669"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039669","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["443787","443781","443789","443779","443782","443778","443783","443788","443780","443784","443785","443786"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Model support system using an industrial robot in low-speed wind tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"23","bibliographicPageStart":"1","bibliographicVolumeNumber":"666","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所の突風風洞では、HOPE開発のための一翼を担う小型自動着陸実験機(ALFLEX:Automatic Landing Flight Experiment)の着陸時空力特性を把握するための地面効果試験を実施した。しかし、地面効果試験において従来の風洞の模型支持方式では、風洞模型を着陸時の姿勢と速度に準じて上下方向に制御することは不可能である。そこで、新たな風洞模型支持装置として産業用ロボットの機構と機能に着目し、これを用いた風洞模型支持システムと風洞試験方法を開発した。本システムでは、風洞模型を要求に応じて迎角、横滑り角、回転角を持った姿勢を設定できるほか、指定した位置へ迅速に移動させることができる。本システムを用いたALFLEXの風洞試験では、従来の低速風洞試験と共に地面効果試験が効率的に実施されただけでなく、最近注目されている動的試験データの取得が可能になるなど、新しい展開の風洞試験方法の可能性を示すことができた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To support the test model and provide a means of changing the attitude and the position, a test on the use of an industrial robot was performed in the NAL gust wind tunnel. For the model support system using a robot, the functional tests were made and aerodynamic characteristics tests at a low-speed wind and ground effect tests were conducted using the 8.9 percent scale model of HOPE (H-2 Orbiting Plane) ALFLEX (Automatic Landing Flight Experiment) vehicle. The obtained data were compared with the results from the same model supported by the sting of a conventional type. This report mainly describes the functional performance of the model support system using the robot and the influence of the robot's arm on the wind flow. The results indicated that the present model support system is very useful to move the model quickly in various directions in the wind tunnel. It was also suggested that the present model support system can be used for dynamic wind tunnel tests and can be recognized as one of the advanced technologies relating to wind tunnel tests.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000089000","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 TM-666","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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":"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 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":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤枝, 郭俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中安, 英彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"匂坂, 雅一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujieda, Hirotoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","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":"naltm00666.pdf","filesize":[{"value":"3.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00666.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39669/files/naltm00666.pdf"},"version_id":"e904d86a-4782-492a-87fb-a8b6dbb3d7da"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持システム","subitem_subject_scheme":"Other"},{"subitem_subject":"産業用ロボット","subitem_subject_scheme":"Other"},{"subitem_subject":"地面効果","subitem_subject_scheme":"Other"},{"subitem_subject":"自動着陸実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"迎え角","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボット制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボット風防","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"industrial robot","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground effect","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":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attack angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robot controller","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robot canopy","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":"産業用ロボットを用いた風洞模型支持システム","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"産業用ロボットを用いた風洞模型支持システム"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39669","relation_version_is_last":true,"title":["産業用ロボットを用いた風洞模型支持システム"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:59.707771+00:00"}