{"created":"2023-06-20T15:11:36.234960+00:00","id":41285,"links":{},"metadata":{"_buckets":{"deposit":"fe079256-1437-41b6-8fb5-e5f2f369dd08"},"_deposit":{"created_by":1,"id":"41285","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41285"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041285","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489244","489245"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Proceedings of the 62nd and 63rd Workshop on Wind Tunnel Research"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"154","bibliographicPageStart":"1","bibliographicVolumeNumber":"45","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論集では風洞試験、測定について、以下のことを論じている。遷音速動安定試験、ストラット支持干渉、マッハ数分布、感圧塗料、圧力分布、ブレード翼端形状、Active Flap効果、有翼宇宙往還機型模型、低騒音モデルロータ、風洞気流検定、高温衝撃風洞、推力検定、セミフリージェット試験法、および垂直離着陸輸送機模型。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this reports the following topics on wind tunnel measurements and tests are described: dynamic stability tests at a transonic wind tunnel, interference in strut mounting, Mach number distribution, pressure sensitive paints, pressure distribution, blade tip shape, active flap effects, a winged reentry space vehicle model, aeroacoustic model rotor, flow quality evaluation, the high enthalpy shock tunnel, thrust calibration, semi-freejet tests and a vertical take off and landing passenger transport model.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028634000","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 SP-45","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":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"航空宇宙技術研究所"}],"nameIdentifiers":[{"nameIdentifier":"489244","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"National Aerospace Laboratory","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"489245","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0000045.pdf","filesize":[{"value":"51.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0000045.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41285/files/nalsp0000045.pdf"},"version_id":"8b44e9d9-0c0c-4ec2-bb1e-f8b14c61a048"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"突風風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"ストラット支持","subitem_subject_scheme":"Other"},{"subitem_subject":"支持干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数分布","subitem_subject_scheme":"Other"},{"subitem_subject":"感圧塗料","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"ブレード","subitem_subject_scheme":"Other"},{"subitem_subject":"翼端形状","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"アクティブフラップ効果","subitem_subject_scheme":"Other"},{"subitem_subject":"有翼宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"模型","subitem_subject_scheme":"Other"},{"subitem_subject":"低騒音モデルロータ","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gust wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"strut mounting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mounting interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure sensitive paint","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade tip shape","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"active flap effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"winged reentry space vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroacoustic model rotor","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 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