{"_buckets": {"deposit": "45e0604f-3f19-4795-9983-09ca931722cc"}, "_deposit": {"created_by": 1, "id": "6143", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6143"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006143", "sets": ["1052", "1891"]}, "author_link": ["30745", "30743", "30750", "30748", "30747", "30744", "30749", "30746"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル（英）", "attribute_value_mlt": [{"subitem_alternative_title": "A numerical simulation of shear coaxial LOX/GH2 jet flame"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-02-28", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "70", "bibliographicPageStart": "65", "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": "Numerical simulation of liquid oxygen/gaseous hydrogen rocket engine combustor is conducted to investigate the flame structure under supercritical pressure. A preliminary result by an axisymmetric numerical simulation with detailed chemistry is shown for a single shear coaxial injector element which follows the experiment by Mayer and Tamura. A real gas effect under supercritical pressure is accounted for by van der Waals equation of state. A fine mesh system with minimum mesh spacing of 5 micrometers is employed to resolve a thin reaction layer under high pressure environment. A stable flame, though unsteady, is obtained by the present simulation. Fundamental features of the flame are clarified by a brief and short-term (for 0.8 ms) observation of the simulated result. Small eddies, which are generated intermittently at the upper corner of the LOX post tip, interact and coalescence with their neighboring eddies while convecting downstream. A recirculation zone near the LOX post tip drives the GH2 flow toward the LOX stream, which anchors the flame and results in a stationary combustion. The flame edge attaches to the LOX post tip and non-premixed combustion occurs. The flame thickness is less than 0.1 mm. No local extinction is observed during the simulation. The present simulation has succeeded to capture the unsteady flame with very thin reaction layer at supercritical pressure.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049212010", "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_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "無機及び物理化学"}, {"subitem_text_value": "流体力学及び熱伝導"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 特別資料"}]}, "item_5_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "item_5_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部"}]}, "item_5_text_7": {"attribute_name": "著者所属（英）", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "松山, 新吾"}], "nameIdentifiers": [{"nameIdentifier": "30743", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "新城, 淳史"}], "nameIdentifiers": [{"nameIdentifier": "30744", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "溝渕, 泰寛"}], "nameIdentifiers": [{"nameIdentifier": "30745", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小川, 哲"}], "nameIdentifiers": [{"nameIdentifier": "30746", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Matsuyama, Shingo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30747", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shinjo, Junji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30748", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Mizobuchi, Yasuhiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30749", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ogawa, Satoru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30750", "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": "2020-01-16"}], "displaytype": "detail", 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"subitem_subject_scheme": "Other"}, {"subitem_subject": "火炎", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れ場", "subitem_subject_scheme": "Other"}, {"subitem_subject": "数値解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rocket engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "combustion", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supercritical pressure", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "liquid oxygen", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hydrogen", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "coaxial nozzle", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flame structure", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "adiabatic flame temperature", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flame", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow field", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "numerical 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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "ロケットエンジン同軸型噴射器まわりの燃焼シミュレーション", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "ロケットエンジン同軸型噴射器まわりの燃焼シミュレーション"}]}, "item_type_id": "5", "owner": "1", "path": ["1052", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6143", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6143", "relation": {}, "relation_version_is_last": true, "title": ["ロケットエンジン同軸型噴射器まわりの燃焼シミュレーション"], "weko_shared_id": -1}