{"created":"2023-06-20T15:11:27.617150+00:00","id":41120,"links":{},"metadata":{"_buckets":{"deposit":"16a9b300-4091-41ff-9155-9f5b0d271436"},"_deposit":{"created_by":1,"id":"41120","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41120"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041120","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450590","450591"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Wind tunnel investigation of an STOL aircraft model: An effect of engine nacelle shape"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"23","bibliographicPageStart":"1","bibliographicVolumeNumber":"653","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(NAL)で開発されたSTOL(短距離離着陸)実験機の風洞試験用模型に搭載されている模擬エンジンのナセル形状は実機エンジンの8％縮尺のナセルより大幅に長くかつ、ナセル下面の形状が異なっている。そこで、風洞試験により得られた空力データから実機の空気力を推算するため、模擬エンジンと実機エンジンのナセルにかかる空力荷重(推算値)の差よりデータの補正を行っている。この補正の妥当性を検討するため、実機と同一形状の8％縮尺フロースルーナセル(実機型)とSTOL実験機の風洞試験用模型のフロースルーナセル(模型型)を製作し、風洞試験を実施し、これらの結果と、模擬エンジン搭載風試の補正結果との比較検討を行った。その結果、力のデータの補正は大きすぎることおよびモーメントの補正はかなり良好であることが分かった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In initial wind tunnel tests on STOL experimental aircraft developed and researched by the National Aerospace Laboratory, a simulator engine nacelle which is longer and larger than that of 8 percent scales of FJR engines used in actual aircraft, was installed and tested on a model. To estimate ASKA's aerodynamics force data from wind tunnel data, the data was modified to take into account the different shapes of engine nacelle used in the simulated engine and that used in an 8 percent scale FJR (Fan Jet Research) engine. To confirm the adequacy of the modification, wind tunnel tests were conducted on a model with 8 percent scales FJR engine. From the comparison of the present test data with the initial test data and modified data, it was found that the correction of forces was overestimated and the correction of moments was fairly good.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004141000","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-653","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 STOLプロジェクト推進本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory STOL Aircraft Project Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"低速空力技術開発チーム"}],"nameIdentifiers":[{"nameIdentifier":"450590","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Low Speed Aerodynamic Team","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"450591","nameIdentifierScheme":"WEKO"}]}]},"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":"naltm00653.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00653.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41120/files/naltm00653.pdf"},"version_id":"a3ae104f-75ee-4062-b3a6-34a33e426159"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"低速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"短距離離着陸機","subitem_subject_scheme":"Other"},{"subitem_subject":"USB機","subitem_subject_scheme":"Other"},{"subitem_subject":"主翼上面吹き出し高揚力機","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"ナセル","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型","subitem_subject_scheme":"Other"},{"subitem_subject":"形状効果","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジンナセル効果","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジンシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"フロースルーナセル","subitem_subject_scheme":"Other"},{"subitem_subject":"空気取入口","subitem_subject_scheme":"Other"},{"subitem_subject":"風試対実機相関","subitem_subject_scheme":"Other"},{"subitem_subject":"実機外挿","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"short take off and landing aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"USB aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"upper surface blowing aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nacelle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"geometry effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine nacelle effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow through nacelle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air intake","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel full scale correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"full scale extrapolation","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":"STOL全機模型風洞試験:エンジンナセル形状効果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"STOL全機模型風洞試験:エンジンナセル形状効果"}]},"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":"41120","relation_version_is_last":true,"title":["STOL全機模型風洞試験:エンジンナセル形状効果"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:42.046442+00:00"}