{"created":"2023-06-20T15:02:37.282735+00:00","id":31711,"links":{},"metadata":{"_buckets":{"deposit":"0496b066-01e2-48f3-9694-2b75b6fd21ee"},"_deposit":{"created_by":1,"id":"31711","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31711"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031711","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["405839","405840","405838","405841"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Characteristics of Wing-Body Combinations at Hypersonic Speed"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-02","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_A","bibliographicPageEnd":"81","bibliographicPageStart":"67","bibliographicVolumeNumber":"13","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本報告は鈍頭円錐をnose coneにもつ翼胴結合体の極超音速空力特性に関する風洞実験の結果である。実験はnose cone,胴体及び翼胴結合体のそれぞれに対して主流マッハ数8に関して行なわれ,小迎角における飛翔体の3分力空力特性か天秤で測定され,翼胴干渉効果か定量的に明らかにされている。小迎角の範囲内ては翼胴結合体の揚力及び縦揺れモーメント係数は迎角に対してほほ直線的に変化し,胴体の円筒部分に発生する揚力は肩の直近下流に限られ,その値は揚力係数傾斜にして高々03てある。無揚力干渉抗力はnose bluntnessの増加に伴なって著しく減少し,その値は翼の平面形に強く依存しており,台形翼よりは三角翼の方か小さく,アスペクト比の小さい翼程小さくなる。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Present paper gives detailed results of a wind tunnel test on aerodynamic characteristics of wing-body combinations at hypersonic speed. The experiment is made for nose cones, cone-cylinders and wing-body combinations, respectively, at free stream Mach number of 8, and 3 components aerodynamic characteristics at small angles of attack are measured to clarify the effect of wing-body interference It is shown that, in the range of small angles of attack, lift and pitching-moment coefficients pertinent to wing-body combinations are almost linear to the angle of attack and the lift coefficient slope appropriate to the cylinder part of the body is 0.3 at maximum. Zero lift drag increment due to wing-body interference is found to decrease considerably with increase of nose bluntness, depending seriously upon the wing plan form, and it is concluded that the interference drag is small for triangular wings with low aspect ratio.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124732000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"辛島, 桂一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 清"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KARASHIMA, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SATO, Kiyoshi","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124732.pdf","filesize":[{"value":"620.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124732.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31711/files/SA0124732.pdf"},"version_id":"5a07aaf2-e6ff-4b26-be3d-4db36c7ad5ab"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"翼胴結合体の極超音速空力特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"翼胴結合体の極超音速空力特性"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"31711","relation_version_is_last":true,"title":["翼胴結合体の極超音速空力特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:52:43.404764+00:00"}