{"created":"2023-06-20T15:11:36.618176+00:00","id":41293,"links":{},"metadata":{"_buckets":{"deposit":"fdabdd89-65dd-4a18-b790-087710453ed7"},"_deposit":{"created_by":1,"id":"41293","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41293"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041293","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489315","489313","489314","489312"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flutter of winged re-entry space vehicle model including yawing-mode effects"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"78","bibliographicPageStart":"73","bibliographicVolumeNumber":"45","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"有翼宇宙往還機打ち上げ形態において、ロケットおよびアダプタの影響をヨー/ロールモードとして模擬し、この自由度を有する特殊な支持装置を製作した。チップフィン翼全機模型をこの支持装置に搭載し、航技研の遷音速風洞でフラッタ実験を行った。その結果、振動特性によってはヨーモードが連成するフラッタの発生が確認され、クリティカルになる可能性があることがわかった。また一部数値解析を行ったので併せて報告する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The effect of the rocket and adapter for the launch condition of a winged re-entry space vehicle was simulated as the yaw or roll mode, and the specific supporting apparatus with this degree of freedom was manufactured. The whole body model of the tip-fin wing type was loaded on the supporting apparatus, and the flutter experiment was carried out at the NAL Transonic Wind Tunnel. As a result, it was confirmed that the flutter coupled by the yawing mode was generated depending on some vibration properties and that the flutter could become critical. A numerical analysis was conducted partially and its result was also reported.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028634008","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 SP-45","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":"0289-260X","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":"AN10097345","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"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"甲斐, 高志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kai, Takashi","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0045008.pdf","filesize":[{"value":"1.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0045008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41293/files/nalsp0045008.pdf"},"version_id":"b316f4b2-cca3-4835-a57f-8d20c0017ca1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"有翼宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"チップフィン翼","subitem_subject_scheme":"Other"},{"subitem_subject":"ヨーイングモード","subitem_subject_scheme":"Other"},{"subitem_subject":"振動試験","subitem_subject_scheme":"Other"},{"subitem_subject":"固有モード","subitem_subject_scheme":"Other"},{"subitem_subject":"NAL","subitem_subject_scheme":"Other"},{"subitem_subject":"機型模型","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"アダプタ","subitem_subject_scheme":"Other"},{"subitem_subject":"winged space reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supporting apparatus","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tip fin wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"yawing mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"natural mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NAL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vehicle model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"adapter","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":"有翼宇宙往還機型模型のヨーイングモードが影響するフラッタ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"有翼宇宙往還機型模型のヨーイングモードが影響するフラッタ"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41293","relation_version_is_last":true,"title":["有翼宇宙往還機型模型のヨーイングモードが影響するフラッタ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:52.251771+00:00"}