{"created":"2023-06-20T15:15:21.597067+00:00","id":45433,"links":{},"metadata":{"_buckets":{"deposit":"def8a25c-9fed-4c64-8f55-eefe28639bb5"},"_deposit":{"created_by":1,"id":"45433","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45433"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045433","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474799","474800"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Yawing Mode Flutter of Non-Planar Wing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"13","bibliographicVolumeNumber":"1451","bibliographic_titles":[{"bibliographic_title":"独立行政法人航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1451","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ロケットの先端に搭載されて打ち上げられる有翼宇宙往還機が，チップフィンのような非平面形態翼である場合，打ち上げロケットとの結合部やロケット自体の弾性による横モード（ヨーイングモード）が，有翼宇宙往還機のフラッタ特性に影響することが考えられる。そこでヨーイングモードを有する特殊なスティング式支持装置に，全機模型を搭載して航技研の遷音速風洞でフラッタ実験を行った。併せてDPM(Doublet-Point Method)を用いてフラッタ解析を行い，ヨーイングモードが連成するフラッタの特性を調べたので報告する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"If a winged reentry space vehicle with non-planar wings such as a tip-fin is attached atop a launch rocket, lateral mode oscillation due to an attachment between the vehicle and the rocket and/or the rocket itself may have an effect on the flutter characteristics of the wings. A particular supporting system was developed for wind tunnel tests, which had a yawing elasticity as a lateral mode. Flutter experiments were conducted in NAL-TWT. Flutter characteristics were also computed by with the doublet-point method (DPM). Numerical results are consistent with experimental results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1451000","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 TR-1451","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":"1347-4588","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":"AN00311347","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構造材料研究センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Structures and Materials Research Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{"nameIdentifier":"474799","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KANDA, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"474800","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr0001451.pdf","filesize":[{"value":"548.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001451.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45433/files/naltr0001451.pdf"},"version_id":"0fdfb847-7e09-4d1d-a3c1-c2f5cdf64d03"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Flutter; Reentry Space Vehicle; Yawing Mode; Wind Tunnel Test; Doublet-Point Method","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":"非平面翼のヨーイングモードフラッタ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非平面翼のヨーイングモードフラッタ"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45433","relation_version_is_last":true,"title":["非平面翼のヨーイングモードフラッタ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:39:28.854621+00:00"}