{"created":"2023-06-20T15:13:50.801640+00:00","id":43818,"links":{},"metadata":{"_buckets":{"deposit":"a497a52d-ca56-48ac-9d1e-bef0b121cae1"},"_deposit":{"created_by":1,"id":"43818","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43818"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043818","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465781","465783","465782","465780"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Tests of an Air Inlet Model for Turbofan Engine (Supplement)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1972-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"21","bibliographicVolumeNumber":"235","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_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The small-scale model adopted in NAL TM-185 is modified and tested. The revised configuration with the diffuser annulus unchanged is of rotating-lip type with fixed-lead- ing-edge ring (auxiliary ports being shifted forward in revision), and has a highlight dia- meter 10% larger than the original one.  The test results are as follows: 1) At zero flight speed without cross wind, the total-pressure recovery attains 98% with auxiliary passages closed and 99% with auxiliary ports open, when the mean axial flow velocity equals 120 m/s at the fan face. 2) On the model with the auxiliary passages dismissed in a cross wind, a tail wind exerts more influence than head wind. When a one-ring-type ring vane is inserted into the  diffuser, the total-pressure distortion is moderated. However, the data has shown that  more research is needed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0235000","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-235","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原動機部"},{"subitem_text_value":"慶応義塾大学工学部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"近藤, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長谷川, 聡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KONDO, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASEGAWA, Satoshi","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00235.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00235.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43818/files/naltm00235.pdf"},"version_id":"2f3e7179-d373-47c1-bb54-5b657c42c05e"}]},"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":"推進エンジン用空気取入口の予備実験(続報)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"推進エンジン用空気取入口の予備実験(続報)"}]},"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":"43818","relation_version_is_last":true,"title":["推進エンジン用空気取入口の予備実験(続報)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:22.319471+00:00"}