{"created":"2023-06-20T14:39:40.499409+00:00","id":6433,"links":{},"metadata":{"_buckets":{"deposit":"bdffd21b-33f8-4700-bf6f-3ff110e7cd44"},"_deposit":{"created_by":1,"id":"6433","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6433"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006433","sets":["1887:1891","9:789:1067:1071"]},"author_link":["32677","32681","32682","32674","32675","32672","32679","32673","32678","32676","32671","32680"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Preliminary report of the starting and stopping loads data in the JAXA 1 m x 1 m supersonic wind tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"67","bibliographicPageStart":"61","bibliographicVolumeNumber":"JAXA-SP-04-014","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第73回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 73rd Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"吹出式の超音速風洞では、風洞の起動および停止時に模型に大きな衝撃荷重が加わり、古くから問題となっている。これは、風洞起動／停止時に上下(左右)非対称の衝撃波が模型上を通過することに起因する。本報告では、JAXA1m×1m超音速風洞における様々な試験で取得してきた風洞起動／停止荷重データを整理し、文献のデータと比較したのでその結果を述べる。また、風洞起動／停止荷重計測用に製作した模型(AGARD-Bの類似模型)を用い、種々のパラメータ(P(sub 0)、ロール角φ、翼の有無)を変化させ、その影響を調査したので併せて報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048471009","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: JAXA-SP-04-014","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"航空宇宙技術振興財団"},{"subitem_text_value":"IHIエアロスペースエンジニアリング"},{"subitem_text_value":"IHIエアロスペースエンジニアリング"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Foundation for Promotion of Japanese Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Engineering Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Engineering Co. 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