{"created":"2023-06-20T15:07:49.606093+00:00","id":37190,"links":{},"metadata":{"_buckets":{"deposit":"d913bb3c-ab83-4e99-a892-895675e4f815"},"_deposit":{"created_by":1,"id":"37190","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37190"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037190","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479431","479441","479438","479435","479426","479440","479429","479427","479432","479428","479439","479434","479437","479430","479433","479436"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A try of high angle of attack test by model mounting from a crooked tail sting in NAL gust wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"86","bibliographicPageStart":"79","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":"航空宇宙技術研究所突風風洞において、VTOL(垂直離着陸)機や失速迎角の大きい試験模型など、高迎角までの空力特性を把握するための試験を行なう簡便な方法として、曲がりスティングと6自由度を有するロボットを利用した模型支持法の採用を試みた。今回は本方式による最初の試験として、ALFLEX(小型自動着陸実験)16%模型を用いて設定迎角の可能な範囲や模型支持装置としての強度、剛性など安全上の確認とともに、本支持装置の試験模型の空力特性への影響を把握するために縦3分力測定とベース圧測定試験を行なった。空力特性への影響の程度を知る目安として、本試験で得られた結果を、別途実施された一般的な試験迎角範囲で使用される真っ直ぐなスティングによる同一模型の試験結果と比較検討した。ここでは、その概要について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In NAL gust wind tunnel, an experiment of employing the model supporting method using crooked tail sting and robot with six degree of freedom as a conventional method was made for aerodynamic tests to investigate aerodynamic characteristics up to high elevation angle in such cases of VTOL (Vertical Takeoff and Landing) vehicle, high stalling angle of attack and so on. For the first test of this method, measurement tests of vertical three component internal balance and base pressure were carried out to investigate effects of this model supporting equipment on aerodynamic characteristics of test model, as well as to confirm the safety using 16 percent model of ALFLEX (Automatic Landing Flight Experiment) from the viewpoint of possible range of setting angle of attack, strength and rigidity necessary for model supporting equipment. For measuring the extent of effects of this model supporting equipment on aerodynamic characteristics, the results obtained from this tests were compared with those performed in the other test of same model supported by straight sting used in the range of general test angle of attack. In this paper, the outline of this experiment is reported.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001434008","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"},{"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":"航空宇宙技術研究所"},{"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":"航空宇宙技術研究所"},{"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"},{"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 Aerospace Laboratory"},{"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 Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤枝, 郭俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, ひとし"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"奥山, 政広"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 婦美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 和夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 誠三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujieda, Hirotoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Hitoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okuyama, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Fumiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Seizo","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":"nalsp0038008.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0038008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37190/files/nalsp0038008.pdf"},"version_id":"0a34718a-6e2f-4f24-863b-53dfc857b079"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"突風風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"曲がりスティング","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"高仰角","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"縦3分力測定","subitem_subject_scheme":"Other"},{"subitem_subject":"ベース圧測定","subitem_subject_scheme":"Other"},{"subitem_subject":"スティング","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"gust wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crooked tail sting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model supporting equipment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high attack angle","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":"vertical three component internal balance measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"base pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"NAL突風風洞における曲がりスティングによる高迎角風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"NAL突風風洞における曲がりスティングによる高迎角風洞試験"}]},"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":"37190","relation_version_is_last":true,"title":["NAL突風風洞における曲がりスティングによる高迎角風洞試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:23:48.223051+00:00"}