{"created":"2023-06-20T15:11:28.547667+00:00","id":41140,"links":{},"metadata":{"_buckets":{"deposit":"4724a3bd-b5ad-409c-b6a4-71929b2e7ba2"},"_deposit":{"created_by":1,"id":"41140","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41140"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041140","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450731","450733","450732","450730"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurement of free-stream properties in the NAL 0.1 m x 0.1 m transonic cryogenic wind tunnel, part 2"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"10","bibliographicPageStart":"1","bibliographicVolumeNumber":"677","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":"集合胴における温度分布とスロット壁に沿った試験部分の静圧分布を測定した。集合胴における温度分布は手で互に交差した2つの熱電対で測定した。集合胴における温度の変化は集合胴の壁に沿った熱的な境界層を除いてプラスマイナス1K以内であった。熱的な境界層の厚さは50ミリ以下であったが、脚部のどの部分よりも厚かった。試験部分の静圧の測定結果は、浮力効果が7.5ミリのAGARD-Bモデルの6カウント分の抗力上昇を引き起こす圧力傾斜を明らかにした。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Temperature distributions at the settling chamber and test section static pressure distributions along the slotted wall are dealt with. Temperature distributions at the settling chamber were measured by two thermocouple probes which were traversed by hand alternately. The variation in temperature at the settling chamber was within +/- 1 K except for the thermal boundary layer along the settling chamber wall. The thermal boundary layer thickness was less than 50 mm, but was more than any other station near the leg. Test section static pressure measurements revealed a pressure gradient whose buoyancy effect causes six counts of drag rise of the 7.5 mm AGARD-B model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004161000","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-677","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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"青木, 竹夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"澤田, 秀夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoki, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawada, Hideo","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":"naltm00677.pdf","filesize":[{"value":"624.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00677.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41140/files/naltm00677.pdf"},"version_id":"487e36fc-a86b-4173-b69f-8f47abed8388"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"航空宇宙技術研究所","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"低温風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"測定","subitem_subject_scheme":"Other"},{"subitem_subject":"熱的境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"浮力効果","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"集合胴","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"スロット壁","subitem_subject_scheme":"Other"},{"subitem_subject":"熱電対","subitem_subject_scheme":"Other"},{"subitem_subject":"温度変化","subitem_subject_scheme":"Other"},{"subitem_subject":"National Aerospace Laboratory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cryogenic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"buoyancy effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"settling chamber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"slotted wall","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermocouple","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature variation","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0.1m×0.1m遷音速低温風洞の気流測定　その2","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研0.1m×0.1m遷音速低温風洞の気流測定　その2"}]},"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":"41140","relation_version_is_last":true,"title":["航技研0.1m×0.1m遷音速低温風洞の気流測定　その2"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:21.581223+00:00"}