{"created":"2023-06-20T15:10:45.155618+00:00","id":40324,"links":{},"metadata":{"_buckets":{"deposit":"fc9b46cc-8eb8-4688-bebe-aee28543137e"},"_deposit":{"created_by":1,"id":"40324","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40324"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040324","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["447352","447351","447353","447350"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effects of rolling elasticity on flutter characteristics at launching configuration of re-entry space vehicle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"1","bibliographicVolumeNumber":"1380","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HOPE-Xの計画が進んでいる。HOPE-Xの打上げ形態の一つにH-2ロケットの先端に搭載される方式が考えられている。このときHOPE-Xの動特性にロケットまたはロケット結合部によるロール弾性モードが含まれる。航技研遷音速風洞にて風洞実験を行った結果、ロール弾性を有する全機模型で翼の逆対称の曲げと捩りモードが連成する逆対称モードフラッタが発生し、ロールフリーの時よりも低い動圧で発生することがわかった。さらに非定常空気にDPM(Doublet-Point Method)を用いたフラッタ解析でもこのことが示された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The experimental winged space vehicle 'HOPE-X' (H-2 Orbiting Plane-X) project is progressing. A elastic-rolling mode may be involved in the dynamic characteristics at the launching configuration of this vehicle which is attached to the H-2 rocket. Flutter experiments of a HOPE-like configuration model were made in a transonic wind tunnel. As a result, a wing bending-torsional mode flutter occurred in anti-symmetric mode. It was observed that the flutter occurred at lower dynamic pressure in the case of elastic support for roll than in the roll-free case. This type of flutter was confirmed by numerical analyzes with the unsteady aerodynamic forces by DPM (Doublet-Point Method).","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001684000","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-1380","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001380.pdf","filesize":[{"value":"4.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001380.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40324/files/naltr0001380.pdf"},"version_id":"3ba4331f-7d1c-4f05-8916-0f963e97bbd4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"打上げ形態","subitem_subject_scheme":"Other"},{"subitem_subject":"ロール弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"振動モード","subitem_subject_scheme":"Other"},{"subitem_subject":"逆対称モードフラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"対称モードフラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"翼曲げモードフラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"翼ねじりモードフラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"launching configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rolling elasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"antisymmetric mode flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"symmetric mode flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing bending mode flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing torsional mode flutter","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":"有翼宇宙往還機打上げ形態におけるロール弾性のフラッタ特性への影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"有翼宇宙往還機打上げ形態におけるロール弾性のフラッタ特性への影響"}]},"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":"40324","relation_version_is_last":true,"title":["有翼宇宙往還機打上げ形態におけるロール弾性のフラッタ特性への影響"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:15:17.487314+00:00"}