WEKO3
アイテム
{"_buckets": {"deposit": "311e97c2-95af-44c0-b81a-10ad93ddc774"}, "_deposit": {"created_by": 1, "id": "37341", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "37341"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00037341", "sets": ["1891", "1915"]}, "author_link": ["480227", "480238", "480226", "480231", "480237", "480228", "480229", "480235", "480230", "480232", "480234", "480239", "480236", "480233"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Comparison between unsteady stage analysis and steady stage analysis for evaluation of aerodynamic performance of single-stage turbine"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1999-02", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "190", "bibliographicPageStart": "185", "bibliographicVolumeNumber": "41", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所特別資料"}, {"bibliographic_title": "Special Publication of National Aerospace Laboratory", "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": "航空宇宙技術研究所 24-26 Jun. 1998 東京 日本", "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": "National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "局所時間刻みを用いたレイノルズ平均化3次元ナビエ・ストークスコードを、NALの数値風洞(NWT)と称される並列スーパコンピュータの利用を目的として拡張した。本研究は高圧タービンの静翼の配列について、定常段解析と非定常段解析の比較に注目した。非定常段解析の結果は定常段解析よりも実験結果と良好な一致を与えた。これは、主に、前者の方が後者よりも、ケーシング近傍の2次流についてより良い予測を与えることによる。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A three dimensional time accurate Reynolds-averaged Navier-Stokes code has been extended for use in a parallel supercomputer called Numerical Wind Tunnel (NWT) developed by the Japanese National Aerospace Laboratory. This study focuses on comparison between steady stage analysis and unsteady stage analysis for a stator rotor configuration of a high pressure turbine. The result of the unsteady stage analysis shows better agreement with experimental data than that of the steady stage analysis. This is mainly attributed to better prediction of secondary flow near the casing by the unsteady stage analysis than the steady stage analysis.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0001958027", "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: NAL SP-41", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory (NAL)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0289-260X", "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": "AN10097345", "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: 航空宇宙技術研究所"}]}, "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_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": "石川島播磨重工業"}, {"subitem_text_value": "石川島播磨重工業"}, {"subitem_text_value": "石川島播磨重工業"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Ishikawajima-Harima Heavy Industries Co Ltd"}, {"subitem_text_language": "en", "subitem_text_value": "Ishikawajima-Harima Heavy Industries Co Ltd"}, {"subitem_text_language": "en", "subitem_text_value": "Ishikawajima-Harima Heavy Industries Co Ltd"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "平井, 健二"}], "nameIdentifiers": [{"nameIdentifier": "480226", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "児玉, 秀和"}], "nameIdentifiers": [{"nameIdentifier": "480227", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "大山, 亜希彦"}], "nameIdentifiers": [{"nameIdentifier": "480228", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "野崎, 理"}], "nameIdentifiers": [{"nameIdentifier": "480229", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "菊地, 一雄"}], "nameIdentifiers": [{"nameIdentifier": "480230", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "西澤, 敏雄"}], "nameIdentifiers": [{"nameIdentifier": "480231", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "松尾, 裕一"}], "nameIdentifiers": [{"nameIdentifier": "480232", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hirai, Kenji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480233", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kodama, Hidekazu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480234", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Oyama, Akihiko", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480235", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nozaki, Osamu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480236", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kikuchi, Kazuo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480237", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nishizawa, Toshio", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480238", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Matsuo, Yuichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480239", "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": "2020-02-10"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "nalsp0041027.pdf", "filesize": [{"value": "390.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 390900.0, "url": {"label": "nalsp0041027.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/37341/files/nalsp0041027.pdf"}, "version_id": "73340020-e2fe-462f-86e9-066b8c66e82a"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "単段タービン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "翼列", "subitem_subject_scheme": "Other"}, {"subitem_subject": "非定常段解析", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力性能", "subitem_subject_scheme": "Other"}, {"subitem_subject": "2次流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ケーシング", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高圧タービン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "動翼", "subitem_subject_scheme": "Other"}, {"subitem_subject": "静翼", "subitem_subject_scheme": "Other"}, {"subitem_subject": "乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "差分法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "TVDスキーム", "subitem_subject_scheme": "Other"}, {"subitem_subject": "H型格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "全変動減少スキーム", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ナビエ・ストークスコード", "subitem_subject_scheme": "Other"}, {"subitem_subject": "single stage turbine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "cascade", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "unsteady stage analysis", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic performance", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "secondary flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "casing", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high pressure turbine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rotor", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "stator", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "turbulence model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "difference method", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "TVD scheme", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "H type lattice", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "total variation diminishing scheme", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Navier Stokes code", "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": "単段タービン性能予測に対する非定常段解析と定常段解析の比較", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "単段タービン性能予測に対する非定常段解析と定常段解析の比較"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/37341", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "37341", "relation": {}, "relation_version_is_last": true, "title": ["単段タービン性能予測に対する非定常段解析と定常段解析の比較"], "weko_shared_id": -1}
単段タービン性能予測に対する非定常段解析と定常段解析の比較
https://jaxa.repo.nii.ac.jp/records/37341
https://jaxa.repo.nii.ac.jp/records/37341276e8ac7-8f4a-43d2-8fe5-309b8a46e4e5
名前 / ファイル | ライセンス | アクション |
---|---|---|
![]() |
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 単段タービン性能予測に対する非定常段解析と定常段解析の比較 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 単段タービン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼列 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非定常段解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力性能 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2次流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ケーシング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高圧タービン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 静翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 差分法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVDスキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H型格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 全変動減少スキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークスコード | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | single stage turbine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cascade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unsteady stage analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic performance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | secondary flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | casing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high pressure turbine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulence model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | difference method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TVD scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H type lattice | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total variation diminishing scheme | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes code | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Comparison between unsteady stage analysis and steady stage analysis for evaluation of aerodynamic performance of single-stage turbine | |||||
著者 |
平井, 健二
× 平井, 健二× 児玉, 秀和× 大山, 亜希彦× 野崎, 理× 菊地, 一雄× 西澤, 敏雄× 松尾, 裕一× Hirai, Kenji× Kodama, Hidekazu× Oyama, Akihiko× Nozaki, Osamu× Kikuchi, Kazuo× Nishizawa, Toshio× Matsuo, Yuichi |
|||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 41, p. 185-190, 発行日 1999-02 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 24-26 Jun. 1998 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 局所時間刻みを用いたレイノルズ平均化3次元ナビエ・ストークスコードを、NALの数値風洞(NWT)と称される並列スーパコンピュータの利用を目的として拡張した。本研究は高圧タービンの静翼の配列について、定常段解析と非定常段解析の比較に注目した。非定常段解析の結果は定常段解析よりも実験結果と良好な一致を与えた。これは、主に、前者の方が後者よりも、ケーシング近傍の2次流についてより良い予測を与えることによる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A three dimensional time accurate Reynolds-averaged Navier-Stokes code has been extended for use in a parallel supercomputer called Numerical Wind Tunnel (NWT) developed by the Japanese National Aerospace Laboratory. This study focuses on comparison between steady stage analysis and unsteady stage analysis for a stator rotor configuration of a high pressure turbine. The result of the unsteady stage analysis shows better agreement with experimental data than that of the steady stage analysis. This is mainly attributed to better prediction of secondary flow near the casing by the unsteady stage analysis than the steady stage analysis. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001958027 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-41 |