{"_buckets": {"deposit": "aa2374a8-3053-4839-a33f-60754341f043"}, "_deposit": {"created_by": 1, "id": "4248", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "4248"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00004248", "sets": ["896", "1537", "1881", "1891"]}, "author_link": ["18550", "18553", "18551", "18552", "18555", "18554"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル（英）", "attribute_value_mlt": [{"subitem_alternative_title": "A High Accuracy Flow Analysis Method using Residual Cutting Algorithm"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2013-03-29", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "48", "bibliographicPageStart": "43", "bibliographicVolumeNumber": "JAXA-SP-12-010", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012", "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": "第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県", "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": "44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録（英）", "attribute_value_mlt": [{"subitem_description": "The goals of the present study are to develop a numerical flow analysis method based on a high-accuracy algorithm and to simulate flow field around realistic shape like cascades of gas turbines with numerical method. In this paper, a high-accuracy algorithm which forms the basis of the high-accuracy flow simulation is described. In this algorithm, firstly the pressure gradient in the source term of Poisson equation is corrected so that the residual of the equation of continuity in the next time should be zero. Then, the pressure fields in next time iteration are calculated based on the corrected pressure gradient. Finally, the momentum conservation equations are solved with the new pressure field. The target accuracy is realized by repeating the procedure above. In our numerical solver, Residual Cutting Algorithm, which JAXA has developed, is adopted as matrix solver. Three cases of incompressible flow are analyzed to verify our numerical code\"\"\" ; Poiseuille flow between parallel flat plates, flow in a cascade of flat plate blades, and square cavity flow. The results are good and the applicability of our high-accuracy method for simulated flow fields is demonstrated.", "subitem_description_type": "Other"}]}, "item_5_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_5_description_19": {"attribute_name": "内容記述（英）", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains color illustrations", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0061958008", "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-12-010", "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(JAXA)"}]}, "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_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_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "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_41": {"attribute_name": "jaxa出版物シリーズ", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物シリーズ: 015"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 521"}]}, "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(JAXA)"}, {"subitem_text_value": "宇宙航空研究開発機構航空本部推進システム研究グループ(JAXA)"}, {"subitem_text_value": "エイ・エス・アイ総研"}]}, "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 (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Propulsion Systems Research Group,　Institute Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Advanced Science \u0026 Intelligence Research Institute Corp."}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "菊地, 一雄"}], "nameIdentifiers": [{"nameIdentifier": "18550", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "西澤, 敏雄"}], "nameIdentifiers": [{"nameIdentifier": "18551", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "関根, 義人"}], "nameIdentifiers": [{"nameIdentifier": "18552", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kikuchi, Kazuo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "18553", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nishizawa, Toshio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "18554", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sekine, Yoshihito", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "18555", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", 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"permalink_uri": "https://jaxa.repo.nii.ac.jp/records/4248", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "4248", "relation": {}, "relation_version_is_last": true, "title": ["残差切除法を用いた高精度流れ解析手法について"], "weko_shared_id": -1}