{"created":"2023-06-20T15:11:27.797946+00:00","id":41124,"links":{},"metadata":{"_buckets":{"deposit":"1f5b9e54-400b-40bb-86ad-f2f6297ef82d"},"_deposit":{"created_by":1,"id":"41124","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41124"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041124","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["450626","450633","450631","450628","450632","450624","450629","450630","450622","450627","450625","450623"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Static pressure measurements on the surface of the model strut and the sidewall in the NAL 2mX2m transonic wind tunnel test section"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"15","bibliographicPageStart":"1","bibliographicVolumeNumber":"657","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":"航技研(NAL)遷音速風洞の全機模型支持装置は、超音速(約1.4M)において、厳しい振動を起こす。この原因を見出すために支持装置模型を用いてその表面の静圧分布を測定した。この支持装置模型は、全機模型支持装置を模擬して作られこれを基準形態として他に2つの形態で、半截模型測定部において全機模型測定部の支持装置と同じ位置に取付けられ、試験された。また、側壁開度の影響を調べる試験も行われた。その結果、M∞=1.3を越えると、ストラット表面に非定常な流れを生じ、圧力分布上に不規則な変化が表われ、また、側壁開度を増すと、支持装置模型および側壁上の流れが大幅に減速された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To identify the source of severe aerodynamical vibration encountered with the complete airplane model support system of the NAL 2m x 2m Transonic Wind Tunnel at higher supersonic Mach numbers, static pressure distributions were measured on the surface of the model strut and the sidewall. The model strut is installed in the Semispan model Test Section which originally has a free space at the portion corresponding to the model support system position in the complete airplane model Test Section. Three model strut configurations were tested, and the effects of the sidewall streamwise divergence were observed by the divergence angle from the standard one sixth deg to one quarter deg and one third deg.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004145000","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-657","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"},{"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"},{"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":"小池, 陽"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"細江, 信幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 正剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小國, 保男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"唐沢, 敏夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koike, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosoe, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Seigo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oguni, Yasuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Karasawa, Toshio","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":"naltm00657.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00657.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41124/files/naltm00657.pdf"},"version_id":"a5618e4b-dc57-47d6-a8a4-d01c77244b5c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞気流特性","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞気流振動","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型振動","subitem_subject_scheme":"Other"},{"subitem_subject":"空力的振動","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力計測","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞拡散胴部流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞内非定常流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"第2スロート部","subitem_subject_scheme":"Other"},{"subitem_subject":"気流特性","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常衡撃波特性","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞側壁","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数分布","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel flow vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamical vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel diffuser flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel unsteady flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"second throat","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady shock characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel side wall","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number distribution","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":"遷音速風洞における測定部模型支持装置周りの気流特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速風洞における測定部模型支持装置周りの気流特性"}]},"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":"41124","relation_version_is_last":true,"title":["遷音速風洞における測定部模型支持装置周りの気流特性"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:38.034134+00:00"}