{"_buckets": {"deposit": "d2e8be6e-5c1f-42e4-8f18-d57422ff0eb6"}, "_deposit": {"created_by": 1, "id": "6137", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6137"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006137", "sets": ["1052", "1891"]}, "author_link": ["30703", "30709", "30710", "30705", "30706", "30701", "30704", "30708", "30702", "30707"], "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-02-28", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "34", "bibliographicPageStart": "29", "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": "Helicopters are used in various fields such as EMS (Emergency Medical Service), fire fighting, disaster relief, news report, and so on because of the capabilities of hovering and VTOL. However, noise, cost, and VFR (Vision Flight Rules) problems prevent helicopters from being widely used as a means of inter-city transportation in densely populated area. Prediction of the flow field of helicopter rotors in forward night is regarded as one of the most challenging problems in current computational fluid dynamics. Addition of the fuselage underneath the rotor further amplifies the complexity, requiring the solution of unsteady three-dimensional flows involving multiple bodies in relative motion. The periodic airloads, which is principally due to the rotating main rotor blades, impact the undesirable noise and vibration on the fuselage in the way of a mutual aerodynamic interference. Therefore, elaborate aerodynamic analyses of the rotor-fuselage interaction are needed to understand the physics and as an aid to the designers. In the preset study, three dimensional parallel Euler flow solvers have been developed for the simulation of unsteady rotor-fuselage interaction aerodynamics on both structured and unstructured grids using the ROBIN (ROtor Body INteraction) configuration. Validations with experimental data are conducted by simulating the flows around the ROBIN fuselage. The merit/demerit of each grid system is discussed.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049212004", "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": "航空力学"}, {"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"}, {"subitem_text_value": "宇宙航空研究開発機構"}, {"subitem_text_value": "宇宙航空研究開発機構"}, {"subitem_text_value": "Korea Advanced Inst. of Sci. and Tech."}, {"subitem_text_value": "Korea Advanced Inst. of Sci. and Tech."}]}, "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"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency"}, {"subitem_text_language": "en", "subitem_text_value": "Korea Advanced Institute of Science and Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Korea Advanced Institute of Science and Technology"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "Yang, Choongmo"}], "nameIdentifiers": [{"nameIdentifier": "30701", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "青山, 剛史"}], "nameIdentifiers": [{"nameIdentifier": "30702", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "齊藤, 茂"}], "nameIdentifiers": [{"nameIdentifier": "30703", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nam, Hwajin"}], "nameIdentifiers": [{"nameIdentifier": "30704", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kwon, Ohjoon"}], "nameIdentifiers": [{"nameIdentifier": "30705", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yang, Choongmo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30706", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Aoyama, Takashi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30707", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Saito, Shigeru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30708", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nam, Hwajin", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30709", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kwon, Ohjoon", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "30710", "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", "download_preview_message": "", "file_order": 0, "filename": "49212004.pdf", "filesize": [{"value": "2.5 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 2500000.0, "url": {"label": "49212004.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6137/files/49212004.pdf"}, "version_id": "eaed8548-eeaf-49a3-9fcf-b6545a1b98af"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "ヘリコプター", "subitem_subject_scheme": "Other"}, {"subitem_subject": "胴体", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ROBIN形状", "subitem_subject_scheme": "Other"}, {"subitem_subject": "構造格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "非構造格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "数値解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流速差分分離", "subitem_subject_scheme": "Other"}, {"subitem_subject": "比較", "subitem_subject_scheme": "Other"}, {"subitem_subject": "渦度", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ロータトリム", "subitem_subject_scheme": "Other"}, {"subitem_subject": "表面格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "背景格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "helicopter", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "fuselage", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "robin configuration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "structured grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "unstructured grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "numerical analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flux difference splitting", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "comparison", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "vorticity", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rotor trim", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "surface grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "background grid", "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "Comparison of structured and unstructured grids on generic helicopter fuselage with a rotor", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Comparison of structured and unstructured grids on generic helicopter fuselage with a rotor", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1052", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6137", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6137", "relation": {}, "relation_version_is_last": true, "title": ["Comparison of structured and unstructured grids on generic helicopter fuselage with a rotor"], "weko_shared_id": -1}