WEKO3
アイテム
{"_buckets": {"deposit": "2ed26ac1-fafc-4fe7-b6f2-6e91b2ee91d1"}, "_deposit": {"created_by": 1, "id": "6198", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6198"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006198", "sets": ["1056", "1891"]}, "author_link": ["31069", "31067", "31065", "31070", "31066", "31068"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Study of transition mechanism in a supersonic boundary layer at M = 3 using spatial DNS"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-02-01", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "52", "bibliographicPageStart": "51", "bibliographicVolumeNumber": "JAXA-SP-05-012", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集 第35回・第36回"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Spatial direct numerical simulations are used to study the formation and development of three-dimensional structures in a supersonic flat plate boundary layer, where the free-stream Mach number is three and the Reynolds number at the inlet based on the displacement thickness 1,000. Random disturbances are superimposed on the laminar profile at the inlet plane of the boundary layer computational box. Hairpin vortices are generated in an intermittent manner on a low speed streak downstream after the low/high speed streaks formation. The numerical turbulent velocity fluctuations are in good agreement with the experimental data of the supersonic turbulent boundary layer for M = 2.9.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049208016", "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-05-012", "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": "航空機の設計、試験及び性能"}, {"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": "広島大学 大学院工学研究科"}, {"subitem_text_value": "広島大学 大学院工学研究科"}, {"subitem_text_value": "広島大学 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": "Hiroshima University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Hiroshima University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Hiroshima University Graduate School of Engineering"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "前川, 博"}], "nameIdentifiers": [{"nameIdentifier": "31065", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "渡辺, 大輔"}], "nameIdentifiers": [{"nameIdentifier": "31066", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "尾崎, 幸玄"}], "nameIdentifiers": [{"nameIdentifier": "31067", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Maekawa, Hiroshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31068", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Watanabe, Daisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31069", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ozaki, Kogen", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31070", "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": "49208016.pdf", "filesize": [{"value": "819.2 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 819200.0, "url": {"label": "49208016.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6198/files/49208016.pdf"}, "version_id": "064a0030-e020-4572-b2a5-bb437b4c86c7"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "境界層遷移", "subitem_subject_scheme": "Other"}, {"subitem_subject": "直接数値シミュレーション", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ヘアピン渦", "subitem_subject_scheme": "Other"}, {"subitem_subject": "超音速境界層", "subitem_subject_scheme": "Other"}, {"subitem_subject": "3次元流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "3次元境界層", "subitem_subject_scheme": "Other"}, {"subitem_subject": "超音速流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "乱流境界層", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流体音響学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "boundary layer transition", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "direct numerical simulation", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hairpin vortex", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic boundary layer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "three dimensional flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "three dimensional boundary layer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "turbulent boundary layer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aeroacoustics", "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": "空間発展DNSによるM=3超音速境界層の遷移機構の研究", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "空間発展DNSによるM=3超音速境界層の遷移機構の研究"}]}, "item_type_id": "5", "owner": "1", "path": ["1056", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6198", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6198", "relation": {}, "relation_version_is_last": true, "title": ["空間発展DNSによるM=3超音速境界層の遷移機構の研究"], "weko_shared_id": -1}
空間発展DNSによるM=3超音速境界層の遷移機構の研究
https://jaxa.repo.nii.ac.jp/records/6198
https://jaxa.repo.nii.ac.jp/records/61985b60d0bb-cc03-4bd7-bc3c-bb043ad02d8b
名前 / ファイル | ライセンス | アクション |
---|---|---|
49208016.pdf (819.2 kB)
|
|
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 | 空間発展DNSによるM=3超音速境界層の遷移機構の研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層遷移 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 直接数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘアピン渦 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流体音響学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer transition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | direct numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hairpin vortex | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aeroacoustics | |||||
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 | Study of transition mechanism in a supersonic boundary layer at M = 3 using spatial DNS | |||||
著者 |
前川, 博
× 前川, 博× 渡辺, 大輔× 尾崎, 幸玄× Maekawa, Hiroshi× Watanabe, Daisuke× Ozaki, Kogen |
|||||
著者所属 | ||||||
広島大学 大学院工学研究科 | ||||||
著者所属 | ||||||
広島大学 大学院工学研究科 | ||||||
著者所属 | ||||||
広島大学 大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Hiroshima University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Hiroshima University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Hiroshima 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: 境界層遷移の解明と制御研究会講演論文集 第35回・第36回 en : JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition 巻 JAXA-SP-05-012, p. 51-52, 発行日 2006-02-01 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Spatial direct numerical simulations are used to study the formation and development of three-dimensional structures in a supersonic flat plate boundary layer, where the free-stream Mach number is three and the Reynolds number at the inlet based on the displacement thickness 1,000. Random disturbances are superimposed on the laminar profile at the inlet plane of the boundary layer computational box. Hairpin vortices are generated in an intermittent manner on a low speed streak downstream after the low/high speed streaks formation. The numerical turbulent velocity fluctuations are in good agreement with the experimental data of the supersonic turbulent boundary layer for M = 2.9. | |||||
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: AA0049208016 | |||||
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-05-012 |