{"created":"2023-06-20T15:11:32.111095+00:00","id":41216,"links":{},"metadata":{"_buckets":{"deposit":"c3e54fc2-7ea1-4553-8c95-e228b3d22e36"},"_deposit":{"created_by":1,"id":"41216","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41216"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041216","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451227","451225","451224","451226"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of combustion flow around a flame holder with hydrogen injection"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"17","bibliographicPageStart":"1","bibliographicVolumeNumber":"1233","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":"ラムジェットエンジン燃焼器用保炎器として、耐熱性の観点から燃料噴出型保炎器が有望と考えられる。その2次元化模型まわりの水素の燃焼を伴う流れの数値シミュレーションコードを開発した。解法としてSIMPLER法、乱流モデルとして明・笠木のk-ε2方程式モデル、燃焼モデルとして渦消散モデルを用いた。このCFD(計算流体力学)コードの詳細といくつかの典型的な計算結果を示す。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the National Aerospace Laboratory, research work on a hydrogen-fueled ramjet engine for the spaceplane is being carried out. As a part of this research, a bluff-body type flame holder with fuel injection was tested at atmospheric conditions and prospective results were obtained for the engine. However, the capability of the experimental facility was limited, and it was difficult to investigate the engine performance over a wide operating range. So a two-dimensional CFD (Computational Fluid Dynamics) code was developed to simulate engine performance over a wide operating range. The code is based on the SIMPLER algorithm, and the power law scheme is used for the discretization of the governing equations. Turbulence is simulated by Myong-Kasagi's low Reynolds number type kappa-epsilon model. Magnussen's eddy dissipation concept is used to simulate the combustion. In this report, details of the CFD code and some typical results of the numerical simulation are described.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004246000","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-1233","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"},{"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"},{"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":"山本, 武"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田丸, 卓"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tamaru, 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":"naltr01233.pdf","filesize":[{"value":"1.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01233.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41216/files/naltr01233.pdf"},"version_id":"f735b494-bea0-4a81-9208-bfd84362c636"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"燃焼器内流れ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジン内流れシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ラムジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"水素燃料噴射","subitem_subject_scheme":"Other"},{"subitem_subject":"保炎器","subitem_subject_scheme":"Other"},{"subitem_subject":"ブラフボデイ流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"エンジン性能解析","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン推進機関","subitem_subject_scheme":"Other"},{"subitem_subject":"ラムジェット燃焼器流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"低レイノルズ数乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"化学種保存","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流消散火炎","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydrogen fuel injection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flame holder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bluff body flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engine performance study","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ramjet combustor flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low Reynolds number turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical species conservation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent diffusive flame","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","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":"燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発"}]},"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":"41216","relation_version_is_last":true,"title":["燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:11:56.448681+00:00"}