{"created":"2023-06-20T15:07:56.702759+00:00","id":37317,"links":{},"metadata":{"_buckets":{"deposit":"60583e45-b17e-40a5-b84a-123b4ab75c8e"},"_deposit":{"created_by":1,"id":"37317","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37317"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037317","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480094","480093","480090","480095","480091","480092"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of SRB separation from H-2 rocket"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"28","bibliographicPageStart":"23","bibliographicVolumeNumber":"41","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":"航空宇宙技術研究所 24-26 Jun. 1998 東京 日本","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":"National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"H-2ロケットにおけるSRB(固体燃料ロケットブースタ)分離の数値解析を運動解析にCFD(計算流体力学)の適用することの妥当性を確認するため運動方程式と連合した時間精度の良好な解法によって行った。流れ場の数値解析にはChimera手法を用いた。幾何学的成分は重ね合わせ格子法で表し、3次元薄層ナビエ・ストークス方程式の解法にはLU-ADI(Lower-Upper Alternating Direction Implicit)法を採用した。H-2ロケットから分離後のSRBの運動は運動方程式を解くことにより求めた。計算結果は実際の飛行におけるSRB分離の映像と比較した。また、現在開発中のH-2AロケットにおけるSRB-Aの分離解析も行った。H-2AロケットにおけるSRB-Aの分離はH-2ロケットの場合と大きく異なった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The phenomena of the SRB (Solid Rocket Booster) separation from the H-2 rocket are simulated numerically by the time-accurate flow solver coupled with the equations of motion for the validation of CFD (Computational Fluid Dynamics) application to dynamic problems. The numerical method for the flow simulation is based on the Chimera technique. Overset grid technique is used to represent the each geometric component and LU-ADI (Lower-Upper Alternating Direction Implicit) procedure is adopted to solve the three dimensional thin layer Navier-Stokes equations. The motion of the SRB after the separation from the H-2 rocket is calculated by solving the equations of motion. Computational result is compared with the picture obtained during the SRB separation in the actual launch. And also the phenomena of the SRB-A separation from the H-2A rocket which is being developed are simulated. The phenomena of the SRB-A separation from the H-2A rocket are quite different from those of the case of the H-2 rocket.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958003","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-41","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":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"宇宙開発事業団"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"大山, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 隆三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oyama, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimizu, Ryuzo","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"H-2ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"SRB分離","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ場解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"LU-ADI手法","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元薄層","subitem_subject_scheme":"Other"},{"subitem_subject":"SRB","subitem_subject_scheme":"Other"},{"subitem_subject":"固体燃料ロケットブースタ","subitem_subject_scheme":"Other"},{"subitem_subject":"上下交互方向陰的差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SRB separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow field analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LU ADI procedure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional thin layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SRB","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"solid rocket booster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lower upper alternating direction implicit procedure","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":"H-2ロケットにおけるSRB分離の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"H-2ロケットにおけるSRB分離の数値解析"}]},"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":"37317","relation_version_is_last":true,"title":["H-2ロケットにおけるSRB分離の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:21:58.774208+00:00"}