{"created":"2023-06-20T15:10:05.299974+00:00","id":39680,"links":{},"metadata":{"_buckets":{"deposit":"5ab60c0e-b301-4e0a-bff6-420ade883f12"},"_deposit":{"created_by":1,"id":"39680","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39680"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039680","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["443863","443862"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"噴流保炎型ラム燃焼器内の乱流場における一般3次元曲線座標での計算機モデル"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-06","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"18","bibliographicPageStart":"1","bibliographicVolumeNumber":"1240T","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":"円筒内に噴流を導入することによって保炎を行う噴流保炎型ラム燃焼器内流れの数値シミュレーションを行うために、一般座標系における3次元計算コードを開発している。現在、この計算コードにより等温流れ場を計算することができる。計算スキームとしてSIMPLER法を用いており、ナビエ・ストークス方程式および低レイノルズ数型κ-εモデルの式を解いている。燃焼器内の流れ場を軸対象と仮定し、円周方向の1/8の部分について計算を行った。その結果得られた流れ模様、速度場、圧力分布を示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A three-dimensional computer code, in arbitrary coordinates, for the simulation of the isothermal flow pattern in a jet induced ram combustor is developed. The Navier-Stokes equation and the equations for a low Reynolds number kappa-epsilon model are solved using the Semi-Implicit Method for Pressure Linked Equations Revised (SIMPLER). The code is used to compute the steady state flow field in the combustor. Computed results showing the formation of vortices, velocity field and pressure distribution are presented.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000100000","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-1240T","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 原動機部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aeroengine Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kumar, S."}],"nameIdentifiers":[{"nameIdentifier":"443862","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kumar, Sanjiv","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"443863","nameIdentifierScheme":"WEKO"}]}]},"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":"naltr1240t.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr1240t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39680/files/naltr1240t.pdf"},"version_id":"3e40f5e2-93b1-4aaa-a773-1d04f55acea8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"乱流場","subitem_subject_scheme":"Other"},{"subitem_subject":"ラム燃焼器","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元曲線座標","subitem_subject_scheme":"Other"},{"subitem_subject":"SIMPLER法","subitem_subject_scheme":"Other"},{"subitem_subject":"改訂圧力リンク方程式半陰法","subitem_subject_scheme":"Other"},{"subitem_subject":"噴流保炎","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"等温流れ場","subitem_subject_scheme":"Other"},{"subitem_subject":"低レイノルズ数κ-εモデル式","subitem_subject_scheme":"Other"},{"subitem_subject":"格子形成","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ram combustor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional curvilinear coordinates","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SIMPLER method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"semi implicit method for pressure linked equations revised","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"jet induced flame stabilizing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"isothermal flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equations for a low Reynolds number kappa epsilon model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"A computer model in general 3-D curvilinear coordinates for the prediction of the turbulent flow field in a jet induced ram combustor","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A computer model in general 3-D curvilinear coordinates for the prediction of the turbulent flow field in a jet induced ram combustor","subitem_title_language":"en"}]},"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":"39680","relation_version_is_last":true,"title":["A computer model in general 3-D curvilinear coordinates for the prediction of the turbulent flow field in a jet induced ram combustor"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:47.428659+00:00"}