{"created":"2023-06-20T15:11:28.024590+00:00","id":41129,"links":{},"metadata":{"_buckets":{"deposit":"c741a29b-9db1-466b-9ec7-16d95627289b"},"_deposit":{"created_by":1,"id":"41129","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41129"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041129","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450651","450653","450654","450648","450649","450650","450655","450652"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On the calibration of six-component internal balances. Part 1: A state of the calibration using dead weight for the NAL-TWT"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"40","bibliographicPageStart":"1","bibliographicVolumeNumber":"663","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":"遷音速風洞計測装置改修の一環として天秤較正装置の更新を行うこととした。本資料は実荷重による天秤較正法、データ処理法、較正結果等遷音速風洞での内装式天秤較正の現状を述べたものであり、この作業を通して新しく導入される装置の評価の目安を得ようとするものである。本較正作業では遷音速風洞で使用頻度の高い天秤2体(国産天秤と外国製天秤)を選び、3種類の天秤特性表示式を適用した。較正データ処理結果による両天秤ともその特性を線形表示した場合明らかに精度不足であった。特に複合負荷でその傾向が顕著であった。一方天秤特性を非線形表示することで精度は力測定試験で許容できる範囲に十分収まっていること、また天秤特性を2次式で評価した場合と3次式で評価した場合の精度の違いおよび2本の天秤の精度の違いは小さいこと等を示した。また較正マトリックスをデルタ翼模型の遷音速風試結果に適用し、天秤特性表示式の違いによる計測結果への影響を示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"NAL (National Aerospace Laboratory) decided to renew the balance calibration rig as a part of the revision program of the instrumentation system for the NAL-TWT (Transonic Wind Tunnel). In this paper, the method of the balance calibration using dead weight, data processing method and calibration results are presented. In the data reduction, three analytical formulae to describe the balance characteristics are applied. The linear expression is poor in accuracy compared with the non-linear formulae including second and third order terms. In the case of non-linear expressions, standard deviations for six balance components are small enough to be acceptable in wind tunnel force tests. The difference in the accuracy between second and third order formulae is small. The present calibration results are applied to the NAL-TWT experimental data using a delta-wing model to evaluate the three formulae for the balance characteristics.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004150000","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-663","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 空力性能部"},{"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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"}]},"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 Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河本, 巌"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 正剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小國, 保男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawamoto, Iwao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Seigo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oguni, Yasuo","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":"naltm00663.pdf","filesize":[{"value":"3.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00663.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41129/files/naltm00663.pdf"},"version_id":"93f99c9c-e234-4087-94cc-d72fa0afce4f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"風洞用天秤較正","subitem_subject_scheme":"Other"},{"subitem_subject":"複合荷重天秤較正","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤較正装置","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤較正方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤荷重変位関係式","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤較正精度","subitem_subject_scheme":"Other"},{"subitem_subject":"内装式六分力天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"1体削り出し型天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"組み立て型天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤零点移動","subitem_subject_scheme":"Other"},{"subitem_subject":"天秤温度ドリフト","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞計測","subitem_subject_scheme":"Other"},{"subitem_subject":"較正試験データ処理","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験データ処理","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel balance calibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combined load balance calibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance calibration rig","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance calibration equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance load deflenction relation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance calibration accuracy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"six component internal balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"machined out balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parts assembled balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"balance zero shift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature dependent balance zero drift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel instrumentation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calibration data processing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel data processing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","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":"内挿式6分力天秤の較正について　第1報:遷音速風洞における実荷重較正の現状","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"内挿式6分力天秤の較正について　第1報:遷音速風洞における実荷重較正の現状"}]},"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":"41129","relation_version_is_last":true,"title":["内挿式6分力天秤の較正について　第1報:遷音速風洞における実荷重較正の現状"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:32.822328+00:00"}