{"created":"2023-06-20T15:10:09.508344+00:00","id":39758,"links":{},"metadata":{"_buckets":{"deposit":"bf486a1a-8807-48ba-945f-adb1a0297a6b"},"_deposit":{"created_by":1,"id":"39758","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39758"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039758","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["444234","444236","444231","444228","444229","444230","444237","444232","444226","444227","444235","444233"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic characteristics of parallel two-stage-to-orbit vehicles using two AGRAD-B standard models in supersonic flows"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"1","bibliographicVolumeNumber":"692","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"並列2段式往還機(TSTO)の超音速領域での飛行と分離を想定して、空力特性がよく知られているAGARD-B模型とその1/2縮尺模型を並行に配置し、2台の模型の迎角と模型間の距離およびマッハ数を変えて空力干渉の試験を行った。各々の模型に組み込まれた6分力天秤で空気力を測定し、単独模型の場合の空力特性と比較した。第1段・第2段模型相互による空力的な干渉の結果、マッハ数・迎角・模型間の距離(垂直および前後方向)によって空力特性(揚力係数および縦揺れモーメント係数)が大きく変化する。従って、第2段機が分離するときに高度の操縦性能が要求される。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To obtain the aerodynamic characteristics of the interaction of parallel Two-Stage-To-Orbit (TSTO) space vehicles in the cruising regions and separation in the supersonic flow, in the range of M(sub infinite) that is equal to or between 1.5 and 2.5, an AGARD (Advisory Group for Aerospace Research and Development)-B standard model and its half-model were tested using two six force balances. By arranging the two models parallel in the same direction and changing the distance and the angle of attack in the range where alpha is greater than or equal to -12 and less than or equal to 12 deg, six aerodynamic force coefficients were measured and compared with the coefficients for a single model. The aerodynamic forces of the upper second stage plane model varied a short distance behind the shock waves of the partner plane. This indicates that sturdy maneuverability is required for a TSTO, especially for the upper second plane during their separation process.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000441000","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 TM-692","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":"0452-2982","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":"AN00314334","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 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原, 亘利"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"榊原, 盛三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河本, 巖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Kiyomichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Nobutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakakibara, Seizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawamoto, Iwao","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm00692.pdf","filesize":[{"value":"10.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00692.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39758/files/naltm00692.pdf"},"version_id":"3e1fdba1-2c5c-4628-96db-d7a990aaa048"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2段式往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD-B標準模型","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行領域","subitem_subject_scheme":"Other"},{"subitem_subject":"空力干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"6分力天秤","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"相互作用","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"操縦性能","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"two stage to orbit vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD B standard model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cruising region","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"six force balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maneuverability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag","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 report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"2台のAGARD-B標準模型による並列二段式往還機の超音速空力特性試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"2台のAGARD-B標準模型による並列二段式往還機の超音速空力特性試験"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39758","relation_version_is_last":true,"title":["2台のAGARD-B標準模型による並列二段式往還機の超音速空力特性試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:30.542695+00:00"}