{"created":"2023-06-20T15:12:34.190644+00:00","id":42424,"links":{},"metadata":{"_buckets":{"deposit":"466c4cea-e2f8-43aa-bd3f-19520199c12a"},"_deposit":{"created_by":1,"id":"42424","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"42424"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00042424","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["458317","458318","458316","458315"],"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 vehicles coupling with elastic pitching mode caused by the booster"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2001-02","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"1423","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"有翼宇宙往還機のようにロケットの先端に搭載され打ち上げられる形態では、ロケットやアダプタの弾性変形モードが往還機の動特性に影響を与える可能性があり、フラッタにおいてこのモードを考慮する必要性がある。制御可能なピッチング剛性を有するスティング型支持装置を開発し航空宇宙技術研究所の遷音速風洞で実験を行った結果、ピッチングモードフラッタの発生が確認され、DMP(Doublet-Point Method)を用いたフラッタ解析でもこのフラッタが確認された。実験ではさらに低い動圧で逆対称モードフラッタの発生を確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An elastic pitching mode may be involved in the dynamic characteristics of the launching configuration of a reentry winged space vehicle attached to a rocket. This type of mode should be taken into consideration for flutter analysis, because flutter can be critical in the launch phase. In this experiment a sting support system with controllable pitching rigidity was built and tested in a transonic wind tunnel, resulting in a pitching mode flutter. This flutter mode was also recognized in flutter analysis using the DPM (Doublet-Point Method). It was also found that in the experiments the flutter occurred at low dynamic pressure in antisymmetric mode.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032243000","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-1423","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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 構造研究部"},{"subitem_text_value":"航空宇宙技術研究所 構造研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 哲彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Tetsuhiko","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":"naltr0001423.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001423.pdf","url":"https://jaxa.repo.nii.ac.jp/record/42424/files/naltr0001423.pdf"},"version_id":"4b1ba6b6-a860-4089-8d38-04b98b2d12ff"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"再突入機","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"動力学特性","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"弾性変形","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素法","subitem_subject_scheme":"Other"},{"subitem_subject":"振動","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elastic deformation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite element method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft model","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":"打ち上げ機によるピッチング弾性モードが連成する有翼機のフラッタ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"打ち上げ機によるピッチング弾性モードが連成する有翼機のフラッタ"}]},"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":"42424","relation_version_is_last":true,"title":["打ち上げ機によるピッチング弾性モードが連成する有翼機のフラッタ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:23:37.646751+00:00"}