{"created":"2023-06-20T15:11:31.884629+00:00","id":41211,"links":{},"metadata":{"_buckets":{"deposit":"b9da1202-4da5-4b57-b4e4-bed93b58e3da"},"_deposit":{"created_by":1,"id":"41211","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41211"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041211","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451191","451190","451188","451189"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurements of longitudinal static aerodynamic coefficients by the cable mount system"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"1","bibliographicVolumeNumber":"1226","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":"当所大型低速風洞(測定部6.5m×5.5m)において、NAL(航空宇宙技術研究所)スペースプレーン模型の静的な縦3分力・空力係数の測定を行うために風洞試験を実施した。この試験では、従来の模型支持法とは異なり、動的風洞試験を目的として開発されたケーブルマウント・システムにより模型を支持して、静的な縦3分力・空力係数の測定を試みた。この測定手法の特徴は、供試模型が2組の極めて細いケーブルで支持されるため、従来のストラットあるいはステイング模型支持方法に比べて、気流に曝される支持部分の抵抗や空力的な干渉が非常に少ないことである。このような特徴から、ケーブルマウント・システムを使った静的な縦3分力・空力係数の測定手法は、飛行試験における方法と類似しており、静的空力係数を取得する有効な手段となる。本報告では、ケーブルマウント・システム、供試模型の概要、静的縦3分力・空力係数の測定方法およびケーブルマウント・システムによる静的縦3分力の測定例について述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The longitudinal static aerodynamic coefficients of an NAL spaceplane model were measured in the NAL 6.5 m x 5.5 m low-speed wind tunnel. The model was supported by a pair of cables, one spanned horizontally and the other vertically (cable mount system). The aerodynamic interference of the cable mount system is generally smaller than that of conventional model support systems such as the strut and sting system. This paper outlines the cable mount system, the model cable mounted, the method used to measure the trimmed longitudinal aerodynamic coefficients and the test results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004241000","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-1226","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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 制御部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"室田, 勝一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"柳原, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murota, Katsuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagihara, Masaaki","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":"naltr01226.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01226.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41211/files/naltr01226.pdf"},"version_id":"c54dc746-3f41-4b63-a38f-1c91320f6322"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"縦静的空力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"空力係数計測","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"模型ワイヤ支持","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーブルマウント模型支持","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"模型姿勢計測法","subitem_subject_scheme":"Other"},{"subitem_subject":"風試模型制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞動的模型試験法","subitem_subject_scheme":"Other"},{"subitem_subject":"自由運動模型支持","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーブルマウントシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"longitudinal static aerodynamic coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic coefficient measurement","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":"model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model wire support","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mount model support","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane aerodynamic characteristics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model attitude measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel dynamic model test method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion free model support","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mount system","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":"ケーブルマウント・システムによる静的縦3分力測定の試み","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ケーブルマウント・システムによる静的縦3分力測定の試み"}]},"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":"41211","relation_version_is_last":true,"title":["ケーブルマウント・システムによる静的縦3分力測定の試み"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:02.075712+00:00"}