WEKO3
アイテム
{"_buckets": {"deposit": "337c45f1-3e1a-41c7-9cb2-f621cd93b42a"}, "_deposit": {"created_by": 1, "id": "34582", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "34582"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00034582", "sets": ["1890", "1901"]}, "author_link": ["419908"], "item_9_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1958-08", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "6", "bibliographicPageEnd": "169", "bibliographicPageStart": "153", "bibliographicVolumeNumber": "24", "bibliographic_titles": [{"bibliographic_title": "東京大學航空研究所報告"}, {"bibliographic_title": "Report/Aeronautical Research Institute, University of Tokyo", "bibliographic_titleLang": "en"}]}]}, "item_9_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Calculations of the effects of pressure gradient and transverse curvature on the boundary layer along slender bodies of revolution are made for allowable body shapes by the series expansion method. Two methods of calculation are presented : the first is the perturbation expansion of flow quantities from the uniform state, and the second is that from the stagnation state. In both cases, allowable body shapes are obtained for the given outer pressure gradient. As an example of the first method, the boundary layer flow along a slender paraboloid of revolution is calculated. The results show that, as already found, the transverse curvature acts on the flow somewhat similarly as a favorable pressure gradient. Further the displacement and the longitudinal curvature effects on the viscous layer is estimated. These effects are found to appear in the second-order terms of the series expansion.", "subitem_description_type": "Other"}]}, "item_9_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: SA2404779000", "subitem_description_type": "Other"}]}, "item_9_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "東京大学航空研究所"}]}, "item_9_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Aeronautical Research Institute, University of Tokyo"}]}, "item_9_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0376-1061", "subitem_source_identifier_type": "ISSN"}]}, "item_9_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA00514444", "subitem_source_identifier_type": "NCID"}]}, "item_9_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: ISASNII"}]}, "item_9_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 宇宙科学研究所"}]}, "item_9_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: 6"}]}, "item_9_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Department of Aeronautics, Faculty of Engineering, Nagoya University."}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "YASUHARA, Michiru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "419908", "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": "2020-01-24"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SA2404779.pdf", "filesize": [{"value": "940.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 940900.0, "url": {"label": "SA2404779.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/34582/files/SA2404779.pdf"}, "version_id": "3cb6ece9-4b28-4f02-8346-bbe7014b9bad"}]}, "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": "departmental bulletin paper", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution", "subitem_title_language": "en"}]}, "item_type_id": "9", "owner": "1", "path": ["1890", "1901"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/34582", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "34582", "relation": {}, "relation_version_is_last": true, "title": ["Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution"], "weko_shared_id": -1}
Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution
https://jaxa.repo.nii.ac.jp/records/34582
https://jaxa.repo.nii.ac.jp/records/34582fe628611-f44b-44cb-ab86-a64c03ab656c
名前 / ファイル | ライセンス | アクション |
---|---|---|
SA2404779.pdf (940.9 kB)
|
|
Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Simultaneous Effects of Pressure Gradient and Transverse Curvature on the Boundary Layer along Slender Bodies of Revolution | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
著者 |
YASUHARA, Michiru
× YASUHARA, Michiru |
|||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautics, Faculty of Engineering, Nagoya University. | ||||||
出版者 | ||||||
出版者 | 東京大学航空研究所 | |||||
出版者(英) | ||||||
出版者 | Aeronautical Research Institute, University of Tokyo | |||||
書誌情報 |
東京大學航空研究所報告 en : Report/Aeronautical Research Institute, University of Tokyo 巻 24, 号 6, p. 153-169, 発行日 1958-08 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Calculations of the effects of pressure gradient and transverse curvature on the boundary layer along slender bodies of revolution are made for allowable body shapes by the series expansion method. Two methods of calculation are presented : the first is the perturbation expansion of flow quantities from the uniform state, and the second is that from the stagnation state. In both cases, allowable body shapes are obtained for the given outer pressure gradient. As an example of the first method, the boundary layer flow along a slender paraboloid of revolution is calculated. The results show that, as already found, the transverse curvature acts on the flow somewhat similarly as a favorable pressure gradient. Further the displacement and the longitudinal curvature effects on the viscous layer is estimated. These effects are found to appear in the second-order terms of the series expansion. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0376-1061 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00514444 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA2404779000 |