WEKO3
アイテム
{"_buckets": {"deposit": "c9c97bab-9440-467d-81fb-1ddde02e2fbd"}, "_deposit": {"created_by": 1, "id": "5530", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "5530"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00005530", "sets": ["976", "1891"]}, "author_link": ["26905", "26901", "26902", "26904", "26906", "26903"], "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-02-29", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "30", "bibliographicPageStart": "27", "bibliographicVolumeNumber": "JAXA-SP-07-026E", "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40回"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of the 40th JAXA Workshop 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": "Flows around a leading-edge slat are investigated experimentally at Reynolds numbers Re less than or equal to 5.2 x 10(exp 5). When the slat operates to suppress the leading-edge stall, a periodic vortex shedding occurs due to the instability of laminar wake of the slat at Reynolds numbers less than 2.1 x 10(exp 5). The Reynolds number variation of the shedding frequency is not unlike that of the circular-cylinder wake at low Reynolds numbers. For Re greater than or equal to 2.3 x 10(exp 5), prominent spectral peaks appear both in the velocity fluctuations and sound-pressure and the frequency of such distinguished noise is found to be proportional to U(sub infinity)(exp 0.84) as reported in the experiment on the sound generation in a single-element airfoil at small angles of attack, suggesting a possibility of feedback loop between the shear layer instability immediately upstream the slat trailing-edge and the generated sound.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063908009", "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-07-026E", "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": "音響学"}]}, "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": "首都大学東京 大学院システムデザイン研究科"}, {"subitem_text_value": "首都大学東京 大学院システムデザイン研究科"}, {"subitem_text_value": "首都大学東京 大学院システムデザイン研究科"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University Graduate School of System Design"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University Graduate School of System Design"}, {"subitem_text_language": "en", "subitem_text_value": "Tokyo Metropolitan University Graduate School of System Design"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "真喜屋, 実寛"}], "nameIdentifiers": [{"nameIdentifier": "26901", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "稲澤, 歩"}], "nameIdentifiers": [{"nameIdentifier": "26902", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "浅井, 雅人"}], "nameIdentifiers": [{"nameIdentifier": "26903", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Makiya, Sanehiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "26904", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Inasawa, Ayumu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "26905", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Asai, Masahito", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "26906", "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": "63908009.pdf", "filesize": [{"value": "987.4 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 987400.0, "url": {"label": "63908009.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/5530/files/63908009.pdf"}, "version_id": "f2bc0511-fb12-4e63-b219-d09ec716e309"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "流れの分布", "subitem_subject_scheme": "Other"}, {"subitem_subject": "前縁スラット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "低レイノルズ数", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高揚力装置", "subitem_subject_scheme": "Other"}, {"subitem_subject": "層流域後流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "渦", "subitem_subject_scheme": "Other"}, {"subitem_subject": "音圧", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力特性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力騒音", "subitem_subject_scheme": "Other"}, {"subitem_subject": "翼型", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れの可視化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "パワースペクトル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow distribution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "leading edge slat", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "low Reynolds number", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high-lift device", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "laminar wake", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "vortex", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "sound pressure", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic characteristic", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic noise", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "airfoil", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow visualization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "power spectrum", "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": "Detailed flow field around a leading-edge slat at low Reynolds numbers", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Detailed flow field around a leading-edge slat at low Reynolds numbers", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["976", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/5530", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "5530", "relation": {}, "relation_version_is_last": true, "title": ["Detailed flow field around a leading-edge slat at low Reynolds numbers"], "weko_shared_id": -1}
Detailed flow field around a leading-edge slat at low Reynolds numbers
https://jaxa.repo.nii.ac.jp/records/5530
https://jaxa.repo.nii.ac.jp/records/55303ef76a4b-8428-42f8-afe2-53e755bcec37
名前 / ファイル | ライセンス | アクション |
---|---|---|
63908009.pdf (987.4 kB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Detailed flow field around a leading-edge slat at low Reynolds numbers | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 前縁スラット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低レイノルズ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高揚力装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層流域後流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 渦 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 音圧 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力騒音 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの可視化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パワースペクトル | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | leading edge slat | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high-lift device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar wake | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vortex | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sound pressure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic noise | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow visualization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | power spectrum | |||||
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 | |||||
著者 |
真喜屋, 実寛
× 真喜屋, 実寛× 稲澤, 歩× 浅井, 雅人× Makiya, Sanehiro× Inasawa, Ayumu× Asai, Masahito |
|||||
著者所属 | ||||||
首都大学東京 大学院システムデザイン研究科 | ||||||
著者所属 | ||||||
首都大学東京 大学院システムデザイン研究科 | ||||||
著者所属 | ||||||
首都大学東京 大学院システムデザイン研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University Graduate School of System Design | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University Graduate School of System Design | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University Graduate School of System Design | ||||||
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40回 en : JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition 巻 JAXA-SP-07-026E, p. 27-30, 発行日 2008-02-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Flows around a leading-edge slat are investigated experimentally at Reynolds numbers Re less than or equal to 5.2 x 10(exp 5). When the slat operates to suppress the leading-edge stall, a periodic vortex shedding occurs due to the instability of laminar wake of the slat at Reynolds numbers less than 2.1 x 10(exp 5). The Reynolds number variation of the shedding frequency is not unlike that of the circular-cylinder wake at low Reynolds numbers. For Re greater than or equal to 2.3 x 10(exp 5), prominent spectral peaks appear both in the velocity fluctuations and sound-pressure and the frequency of such distinguished noise is found to be proportional to U(sub infinity)(exp 0.84) as reported in the experiment on the sound generation in a single-element airfoil at small angles of attack, suggesting a possibility of feedback loop between the shear layer instability immediately upstream the slat trailing-edge and the generated sound. | |||||
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: AA0063908009 | |||||
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-07-026E |