{"created":"2023-06-20T14:39:47.807290+00:00","id":6594,"links":{},"metadata":{"_buckets":{"deposit":"09bda9f9-4356-42b1-a992-ee876c7e16c4"},"_deposit":{"created_by":1,"id":"6594","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6594"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006594","sets":["1887:1891","9:789:1085:1365"]},"author_link":["33745","33747","33744","33746"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Influences of support on measurements with wind tunnel airship models"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"43","bibliographicPageStart":"30","bibliographicVolumeNumber":"JAXA-SP-03-003","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第66回　風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"成層圏プラットフォーム飛行船システム研究開発において、空力推進技術に関わる模型試験が1999年度より要素技術試験として実施されてきた。飛行船は流線形であるため空気力が非常に小さく、風洞試験では模型の支持部分の影響を大きく受けた結果が示された。ここでは、航空宇宙技術研究所6.5m×5.5m低速風洞で実施された船体模型による空力特性の取得試験結果を中心に静水槽試験結果も加えて、計測における模型支持の影響を報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047428005","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-03-003","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 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Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Hitoshi","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":"2020-01-16"}],"displaytype":"detail","filename":"47428005.pdf","filesize":[{"value":"2.1 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test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"strut","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airship","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stratospheric platform","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":"conference 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