{"created":"2023-06-20T14:39:40.630279+00:00","id":6435,"links":{},"metadata":{"_buckets":{"deposit":"62d43152-5d7f-4f57-857e-62b5d5949e74"},"_deposit":{"created_by":1,"id":"6435","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6435"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006435","sets":["1887:1891","9:789:1067:1072"]},"author_link":["32688","32689","32691","32687","32692","32693","32697","32695","32690","32694","32696","32698","32686","32685"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flutter wind tunnel testing with scaled model for SST"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"5","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-04-013","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第72回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 72nd Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXA SSTプロジェクトの第2フェーズとして計画されていたジェット実験機(第1次形状)の弾性模型によるフラッタ試験を、JAXA0.6m×0.6m遷音速フラッタ風洞で実施した。本試験の目的は解析ツールの精度検証のためのデータの取得である。試験供試体には小型超音速ジェット実験機の11％スケール弾性模型を用い、風洞通風域でフラッタを発生させるために翼端後縁に翼型に整形した鉛が取り付けてある。風洞試験により、7点のフラッタポイントを取得し、明確なフラッタバウンダリを捕捉した。また、模型損傷回避策が有効に働き、同一模型でフラッタバウンダリを捕捉することができ、解析ツールの精度検証のための有用なデータを取得した。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048470001","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: 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