{"created":"2023-06-20T14:39:24.023207+00:00","id":6149,"links":{},"metadata":{"_buckets":{"deposit":"52da282d-b736-42ac-8356-2a16d5936193"},"_deposit":{"created_by":1,"id":"6149","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6149"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006149","sets":["1887:1891","9:789:1031:1052"]},"author_link":["30790","30786","30783","30788","30784","30785","30787","30789"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study of numerical simulation of flow over an axisymmetric body in free flight"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"105","bibliographicPageStart":"100","bibliographicVolumeNumber":"JAXA-SP-05-017","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Three-dimensional flow around the slender body, such as aircraft body or rocket cause drastic variation of flow with high angle of attack and have considerable influence on the aerodynamic characteristics. Here the projectile in the inertia flight after thrust of the body has been stopped is studied numerically by a finite difference scheme. This study aims at clarifying the mechanism of free flight, which is affected by the pitching and gravity on body. The initial condition is the flow at steady 'flight' which develops just after the power of engine is shutdown and the vehicle starts free flight with inertia. It has been predicted that in the lower Reynolds number less than 100,000 the flow is symmetric. Therefore, in this numerical study, the flow over a paraboloidal-nose cylinder at pitching rotation in 'free flight' is considered for Reynolds numbers lower than 100,000. The coordinate system fixed on the body, which yields additional terms in Navier Stokes equation. The dual-time pseudo compressibility code is applied for incompressible case, instead PC-TVD scheme for Mach = 0.3 case. The Newton's 2nd law is used with the balance of aerodynamic force and gravity together with angular momentum equation. The aerodynamic coefficients Cd, Cl, Cm are discussed, as well as the trajectory of body.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049212016","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: JAXA-SP-05-017","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"千葉大学 工学部"},{"subitem_text_value":"千葉大学 大学院"},{"subitem_text_value":"千葉大学 大学院"},{"subitem_text_value":"木更津工業高等専門学校"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Chiba University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Chiba University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Chiba University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Kisarazu National College of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"西川, 進栄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"海田, 一哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sun, J."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石出, 忠輝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishikawa, Nobuhide","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaita, Kazuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sun, J.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishide, Tadateru","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":"2020-01-16"}],"displaytype":"detail","filename":"49212016.pdf","filesize":[{"value":"711.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49212016.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6149/files/49212016.pdf"},"version_id":"7fd4396c-133b-4cd5-9581-5810bf53d9be"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"自由飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称物体","subitem_subject_scheme":"Other"},{"subitem_subject":"細長い物体","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"時間発展","subitem_subject_scheme":"Other"},{"subitem_subject":"陰的近似因子化法","subitem_subject_scheme":"Other"},{"subitem_subject":"速度ベクトル","subitem_subject_scheme":"Other"},{"subitem_subject":"free flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"slender body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"time evolution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"implicit approximate factorization method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity vector","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":"慣性飛行時の軸対象物体の流体解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"慣性飛行時の軸対象物体の流体解析"}]},"item_type_id":"5","owner":"1","path":["1052","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6149","relation_version_is_last":true,"title":["慣性飛行時の軸対象物体の流体解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:01:17.324181+00:00"}