{"created":"2023-06-20T15:11:33.043358+00:00","id":41231,"links":{},"metadata":{"_buckets":{"deposit":"0d737274-fa5b-4f7a-b563-63b1e9d0dd60"},"_deposit":{"created_by":1,"id":"41231","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41231"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041231","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451349","451348","451347","451345","451341","451340","451344","451346","451342","451343"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Side force acting on blunted circular cylinder bodies at high angles of attack in supersonic flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"1","bibliographicVolumeNumber":"1255","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ロケット･ブースターおよびロケット自体の安定的な回収のためのデータを得るためにいくつかのマッハ数の超音速流中で、大迎角(32度以上)の鈍頭円柱に作用する横力の測定が行われた。平面と準楕円形を含む鈍頭円柱が横力へのノーズ部の形態の効果を決定するために試験された。平面の円柱に近い高度に鈍い頭の円柱はマッハ数が減少するにつれてより大きな横力を示し、平面の円柱はマッハ数が1.75と2.25の間の狭い領域で大きな横力を示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To obtain data for stable recovery of future rocket boosters and the rocket itself, measurements of side force acting on blunted circular cylinders were carried out at high angles of attack (alpha less than 32 deg.) in supersonic flows of several Mach numbers. The blunted circular heads, including a flat face and semi-elliptic shapes, were tested to determine the effects of nose shapes on side force. Highly blunted bodies close to a flat-faced cylinder show large side force as the Mach number decreases, while a flat-faced cylinder shows large side force in the narrow regions between M(sub infinity) = 1.75 and 2.25.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004262000","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 TR-1255","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"楯, 篤志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉永, 崇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tate, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshinaga, Takashi","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":"naltr01255.pdf","filesize":[{"value":"2.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01255.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41231/files/naltr01255.pdf"},"version_id":"76ca38ca-6042-4db7-8113-c8e63aa702ff"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"大迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"鈍頭","subitem_subject_scheme":"Other"},{"subitem_subject":"横力","subitem_subject_scheme":"Other"},{"subitem_subject":"安定回復","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットブースター","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"ノーズ形状","subitem_subject_scheme":"Other"},{"subitem_subject":"平面円柱","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blunt body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"side force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stabilization recovery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket booster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nose form","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"plane circular cylinder","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":"超音速流中の大迎角鈍頭円柱に作用する横力","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速流中の大迎角鈍頭円柱に作用する横力"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41231","relation_version_is_last":true,"title":["超音速流中の大迎角鈍頭円柱に作用する横力"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:11:38.293030+00:00"}