{"created":"2023-06-20T15:11:36.866613+00:00","id":41298,"links":{},"metadata":{"_buckets":{"deposit":"98bf4c36-464c-4435-9070-d7961232a507"},"_deposit":{"created_by":1,"id":"41298","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41298"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041298","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489371","489364","489363","489361","489362","489367","489365","489358","489368","489370","489359","489360","489366","489369"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The thrust calibration tank for a turbine powered simulator of the transonic wind tunnel in National Aerospace Laboratory"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"135","bibliographicPageStart":"129","bibliographicVolumeNumber":"45","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_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_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":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"STOL(短距離着陸機)実験機「飛鳥」の開発を契機に航技研の遷音速風洞に、TPS(タービン動力模擬エンジン)の推力検定装置を作った。この装置では、TPSの推力を天秤で、またファン流量を音速流量計で精度良く測定する。また、風洞試験時のマッハ数に相当する圧力比を得るために全体が気密容器になっている。本報では、装置の概要、機能と特性、および低速模擬推力検定について説明を行った。本装置の特徴は次の通りである。(1)装置内に音速圧力比、模擬マッハ数に相当する圧力比を設定できる。(2)差圧補償ベローズ機構、6自由度配管干渉除去機構などの採用により天秤への影響をかなり少なくできる。(3)遷音速圧力比の設定には遷音速風洞の排風機かそれと同様の排風能力を持つ機器を使用する必要がある。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Taking the opportunity of the development of STOL (Short Takeoff and Landing) experimental aircraft 'Asuka', the thrust calibration tank for a TPS (Turbine Powered Simulator) was built in the transonic wind tunnel at National Aerospace Laboratory. In this tank, the thrust and fan flow are measured with great accuracy by using a balance and a sonic venturi meter, respectively. Also, the tank itself is made of an airtight container in order to get the pressure ratio equivalent to the Mach number at a wind tunnel test. This paper describes the outline, functions and characteristics of the tank, and also the thrust calibration at the low speed simulation. The characteristics of the tank are as follows. (1) The sonic pressure ratio, and the pressure ratio equivalent to the simulating Mach number can be set up in the tank. (2) The influence on the balance can be reduced to some extent by introducing a differential pressure compensating bellows system, an interference elimination system with six degrees of freedom of piping, etc. (3) It is necessary to use the air-exhaust ventilator of the transonic wind tunnel or an apparatus with the ventilating capacity similar to the ventilator for the fixation of transonic pressure ratio.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028634013","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 SP-45","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":"0289-260X","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":"AN10097345","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"},{"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_3_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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小池, 陽"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"唐沢, 敏夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"末永, 尚史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"半沢, 麻雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野中, 修"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 輝臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"馬場, 滋夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koike, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Karasawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suenaga, Hisashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanzawa, Asao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nonaka, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakaya, Teruomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Baba, Sigeo","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":"nalsp0045013.pdf","filesize":[{"value":"426.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0045013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41298/files/nalsp0045013.pdf"},"version_id":"507668f8-257b-4ad3-9c84-e7fd97af001e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"推力検定タンク","subitem_subject_scheme":"Other"},{"subitem_subject":"NAL","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"TPS","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"ファン流量","subitem_subject_scheme":"Other"},{"subitem_subject":"音速流量計","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"排風機","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力補償ベローズ","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速圧力比","subitem_subject_scheme":"Other"},{"subitem_subject":"干渉消去","subitem_subject_scheme":"Other"},{"subitem_subject":"気密容器","subitem_subject_scheme":"Other"},{"subitem_subject":"短距離着陸機","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust calibration tank","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NAL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TPS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fan flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sonic venturi meter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air exhaust ventilator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure compensating bellows","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic pressure ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interference elimination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airtight container","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"short takeoff and landing","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":"航技研の推力検定装置について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研の推力検定装置について"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41298","relation_version_is_last":true,"title":["航技研の推力検定装置について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:47.203799+00:00"}