{"created":"2023-06-20T15:08:00.029895+00:00","id":37385,"links":{},"metadata":{"_buckets":{"deposit":"29c54fe1-1d2e-4f73-91b8-23676bbffd53"},"_deposit":{"created_by":1,"id":"37385","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37385"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037385","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480476","480482","480485","480484","480483","480479","480478","480477","480480","480481"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Preliminary test with oil flow to clarify the cause of anomaly in control effect on speed-brakes"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"44","bibliographicPageStart":"43","bibliographicVolumeNumber":"42","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_5_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":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_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":"21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"現在進められているHOPE-X(宇宙往還技術試験機)開発において、胴体後方上面に装着されたスピードブレーキの舵効きにおける横・方向特性の変則性が解決すべき要素技術課題になった。この変則性の原因を明らかにするために、予備風試としてALFLEX(小型自動着陸実験)模型を使用し、低速での6分力測定やオイルフロー可視化試験を実施した。左右スピードブレーキ周辺の胴体表面に現れるフローパターンを観察すると、左右スピードブレーキの付け根周りに首飾り渦巻(馬蹄形渦巻)が発生し、この振る舞いが変則性に関連していると推察される。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the development of H-2 Orbiting Plane Experimental (HOPE-X) now in progress, the anomaly in lateral properties of the control effect on the speed brakes at the fuselage rear top has become the elemental technical problem that should be settled. To clarify the cause of the anomaly, low speed six component force measurement and oil flow visualization tests were performed as a preliminary test with the ALFLEX (Automatic Landing Flight Experiment) model. In the flow pattern that appears on the fuselage surface around the right and left speed brakes, necklace eddies (horseshoe type eddies) have been observed around the root of the brake. This phenomenon is considered to be related to the anomaly.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001959005","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: NAL SP-42","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"奥山, 政広"}],"nameIdentifiers":[{"nameIdentifier":"480476","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"青木, 竹夫"}],"nameIdentifiers":[{"nameIdentifier":"480477","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{"nameIdentifier":"480478","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{"nameIdentifier":"480479","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"穂積, 弘一"}],"nameIdentifiers":[{"nameIdentifier":"480480","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Okuyama, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480481","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Aoki, Takeo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480482","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Fujita, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480483","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480484","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hozumi, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"480485","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":"nalsp0042005.pdf","filesize":[{"value":"471.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0042005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37385/files/nalsp0042005.pdf"},"version_id":"5f74b315-1ca5-44bd-91e7-c2e99a21f9ad"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スピードブレーキ","subitem_subject_scheme":"Other"},{"subitem_subject":"舵効き","subitem_subject_scheme":"Other"},{"subitem_subject":"変則性","subitem_subject_scheme":"Other"},{"subitem_subject":"オイルフロー可視化試験","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"6分力測定","subitem_subject_scheme":"Other"},{"subitem_subject":"首飾り渦巻き","subitem_subject_scheme":"Other"},{"subitem_subject":"馬蹄型渦巻き","subitem_subject_scheme":"Other"},{"subitem_subject":"フローパターン","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"speed brakes","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"anormaly","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oil flow visualization test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"six component force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"necklace eddy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"horseshoe type eddy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow pattern","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight Experiment","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"スピードブレーキの舵効きにおける変則性の原因を明らかにするオイルフロー予備試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スピードブレーキの舵効きにおける変則性の原因を明らかにするオイルフロー予備試験"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37385","relation_version_is_last":true,"title":["スピードブレーキの舵効きにおける変則性の原因を明らかにするオイルフロー予備試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:17.263319+00:00"}