WEKO3
アイテム
{"_buckets": {"deposit": "10e131de-a482-4d87-ab79-cd8bff331146"}, "_deposit": {"created_by": 1, "id": "6640", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6640"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006640", "sets": ["1366", "1891"]}, "author_link": ["34023", "34016", "34018", "34020", "34019", "34024", "34014", "34015", "34021", "34022", "34017", "34025"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Numerical simulation of supersonic intake performance for NEXST2 using structured-unstructured zonal approach"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-03-25", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "225", "bibliographicPageStart": "220", "bibliographicVolumeNumber": "JAXA-SP-03-002", "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2003論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In this paper, the numerical simulation method for the supersonic intake performance is proposed. According to the wind tunnel test by NAL, the performance of the supersonic intake integrated to a wing-body was different from the nacelle-only configuration. This result suggested that the intake performance is affected by the wing-body existence. To inspect this difference, the simulations with the nacelle-only configuration and wing-body-nacelle configuration were performed and the calculative results were compared. To obtain higher numerical accuracy of the shock wave, the structured Navier-Stokes code with the low-Reynolds number kappa-epsilon turbulent model were applied to inside the nacelle, while to adapt to the complex geometry of the wing-body-nacelle configuration, the unstructured Euler code was applied to outside the aircraft model. To perform this calculation, the structured-unstructured zonal approach was developed.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047427039", "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-03-002", "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": "航空機の設計、試験及び性能"}, {"subitem_text_value": "航空力学"}, {"subitem_text_value": "数値解析"}]}, "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": "東北大学流体科学研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "東北大学 大学院工学研究科"}, {"subitem_text_value": "東北大学 大学院工学研究科"}, {"subitem_text_value": "東北大学流体科学研究所"}, {"subitem_text_value": "東北大学 大学院工学研究科"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Institute of Fluid Science, Tohoku University"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "Tohoku University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Tohoku University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Fluid Science, Tohoku University"}, {"subitem_text_language": "en", "subitem_text_value": "Tohoku University Graduate School of Engineering"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "金崎, 雅博"}], "nameIdentifiers": [{"nameIdentifier": "34014", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "藤原, 仁志"}], "nameIdentifiers": [{"nameIdentifier": "34015", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "伊藤, 靖"}], "nameIdentifiers": [{"nameIdentifier": "34016", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "藤田, 健"}], "nameIdentifiers": [{"nameIdentifier": "34017", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "大林, 茂"}], "nameIdentifiers": [{"nameIdentifier": "34018", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中橋, 和博"}], "nameIdentifiers": [{"nameIdentifier": "34019", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kanazaki, Masahiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34020", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujiwara, Hitoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34021", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ito, Yasushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34022", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Fujita, Takeshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34023", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Obayashi, Shigeru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34024", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakahashi, Kazuhiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "34025", "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": "47427039.pdf", "filesize": [{"value": "2.3 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 2300000.0, "url": {"label": "47427039.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6640/files/47427039.pdf"}, "version_id": "5bb653c4-7dcd-4e48-9dca-4d2263090391"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "超音速インテーク", "subitem_subject_scheme": "Other"}, {"subitem_subject": "翼・ナセル構成", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "数値シミュレーション", "subitem_subject_scheme": "Other"}, {"subitem_subject": "計算格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Navier-Stokes方程式", "subitem_subject_scheme": "Other"}, {"subitem_subject": "レイノルズ数", "subitem_subject_scheme": "Other"}, {"subitem_subject": "接続法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic intake", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wing nacelle configuration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "numerical simulation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Navier-Stokes equation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Reynolds number", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "zonal approach", "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": "構造-非構造接続法によるNALジェット実験機機体統合超音速インテーク性能解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "構造-非構造接続法によるNALジェット実験機機体統合超音速インテーク性能解析"}]}, "item_type_id": "5", "owner": "1", "path": ["1366", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6640", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6640", "relation": {}, "relation_version_is_last": true, "title": ["構造-非構造接続法によるNALジェット実験機機体統合超音速インテーク性能解析"], "weko_shared_id": -1}
構造-非構造接続法によるNALジェット実験機機体統合超音速インテーク性能解析
https://jaxa.repo.nii.ac.jp/records/6640
https://jaxa.repo.nii.ac.jp/records/6640a5c51e98-df8b-45fa-b81d-1ed13fd3065c
名前 / ファイル | ライセンス | アクション |
---|---|---|
47427039.pdf (2.3 MB)
|
|
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 | 構造-非構造接続法によるNALジェット実験機機体統合超音速インテーク性能解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速インテーク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼・ナセル構成 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Navier-Stokes方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レイノルズ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 接続法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic intake | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing nacelle configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier-Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | zonal approach | |||||
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 | Numerical simulation of supersonic intake performance for NEXST2 using structured-unstructured zonal approach | |||||
著者 |
金崎, 雅博
× 金崎, 雅博× 藤原, 仁志× 伊藤, 靖× 藤田, 健× 大林, 茂× 中橋, 和博× Kanazaki, Masahiro× Fujiwara, Hitoshi× Ito, Yasushi× Fujita, Takeshi× Obayashi, Shigeru× Nakahashi, Kazuhiro |
|||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
東北大学 大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学 大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
東北大学 大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University Graduate School of Engineering | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
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2003論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003 巻 JAXA-SP-03-002, p. 220-225, 発行日 2004-03-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, the numerical simulation method for the supersonic intake performance is proposed. According to the wind tunnel test by NAL, the performance of the supersonic intake integrated to a wing-body was different from the nacelle-only configuration. This result suggested that the intake performance is affected by the wing-body existence. To inspect this difference, the simulations with the nacelle-only configuration and wing-body-nacelle configuration were performed and the calculative results were compared. To obtain higher numerical accuracy of the shock wave, the structured Navier-Stokes code with the low-Reynolds number kappa-epsilon turbulent model were applied to inside the nacelle, while to adapt to the complex geometry of the wing-body-nacelle configuration, the unstructured Euler code was applied to outside the aircraft model. To perform this calculation, the structured-unstructured zonal approach was developed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047427039 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-03-002 |