ログイン
言語:

WEKO3

  • トップ
  • ランキング
To
lat lon distance
To

Field does not validate



インデックスリンク

インデックスツリー

メールアドレスを入力してください。

WEKO

One fine body…

WEKO

One fine body…

アイテム

{"_buckets": {"deposit": "d1bbbda7-49e6-4233-95c5-b052da70110d"}, "_deposit": {"id": "12001", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "12001"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00012001", "sets": ["322"]}, "author_link": ["38013", "38014", "38015", "38016", "38017", "38018"], "item_10_alternative_title_19": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "Effects of Boundary Layer on Supersonic Panel Flutter", "subitem_alternative_title_language": "en"}]}, "item_10_biblio_info_6": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2007-04-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "639", "bibliographicPageEnd": "164", "bibliographicPageStart": "159", "bibliographicVolumeNumber": "55", "bibliographic_titles": [{"bibliographic_title": "日本航空宇宙学会論文集", "bibliographic_titleLang": "ja"}]}]}, "item_10_description_4": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "A fluid-structure coupled computation code has been developed and applied to a panel flutter problem. The flutter velocities and the amplitudes of limit cycle oscillations obtained using the present method agree well with those of Dowell. It is found that the boundary layer over the panel can suppress flutter particularly in the Mach number region between 1.2 and 1.35, the effect of which increases with viscosity. In a 3D problem, good agreement was obtained between computation and experiment.", "subitem_description_language": "en", "subitem_description_type": "Abstract"}]}, "item_10_identifier_60": {"attribute_name": "URI", "attribute_value_mlt": [{"subitem_identifier_type": "HDL", "subitem_identifier_uri": "http://hdl.handle.net/2237/13877"}]}, "item_10_publisher_32": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "日本航空宇宙学会", "subitem_publisher_language": "ja"}]}, "item_10_select_15": {"attribute_name": "著者版フラグ", "attribute_value_mlt": [{"subitem_select_item": "publisher"}]}, "item_10_source_id_7": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1344-6460", "subitem_source_identifier_type": "PISSN"}]}, "item_10_text_14": {"attribute_name": "フォーマット", "attribute_value_mlt": [{"subitem_text_value": "application/pdf"}]}, "item_1615787544753": {"attribute_name": "出版タイプ", "attribute_value_mlt": [{"subitem_version_resource": "http://purl.org/coar/version/c_970fb48d4fbd8a85", "subitem_version_type": "VoR"}]}, "item_access_right": {"attribute_name": "アクセス権", "attribute_value_mlt": [{"subitem_access_right": "open access", "subitem_access_right_uri": "http://purl.org/coar/access_right/c_abf2"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "橋本, 敦", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38013", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "HASHIMOTO, Atsushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38014", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "八木, 直人", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38015", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "YAGI, Naoto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38016", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中村, 佳朗", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38017", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NAKAMURA, Yoshiaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38018", "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": "2018-02-20"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "jjsass_v55_n639.pdf", "filesize": [{"value": "1.1 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_note", "mimetype": "application/pdf", "size": 1100000.0, "url": {"label": "jjsass_v55_n639.pdf", "objectType": "fulltext", "url": "https://nagoya.repo.nii.ac.jp/record/12001/files/jjsass_v55_n639.pdf"}, "version_id": "2d82a86b-b073-4363-a12c-0a6a382292bd"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "Panel Flutter", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Fluid-Structure Coupled Problem", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD-CSD Coupling", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Supersonic Boundary Layer", "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": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "境界層の超音速パネルフラッタへの影響", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "境界層の超音速パネルフラッタへの影響", "subitem_title_language": "ja"}]}, "item_type_id": "10", "owner": "1", "path": ["322"], "permalink_uri": "http://hdl.handle.net/2237/13877", "pubdate": {"attribute_name": "PubDate", "attribute_value": "2010-07-27"}, "publish_date": "2010-07-27", "publish_status": "0", "recid": "12001", "relation": {}, "relation_version_is_last": true, "title": ["境界層の超音速パネルフラッタへの影響"], "weko_shared_id": -1}
  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

境界層の超音速パネルフラッタへの影響

http://hdl.handle.net/2237/13877
http://hdl.handle.net/2237/13877
bad4c458-33d3-4b9b-8896-774cedb077bd
名前 / ファイル ライセンス アクション
jjsass_v55_n639.pdf jjsass_v55_n639.pdf (1.1 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2010-07-27
タイトル
タイトル 境界層の超音速パネルフラッタへの影響
言語 ja
その他のタイトル
その他のタイトル Effects of Boundary Layer on Supersonic Panel Flutter
言語 en
著者 橋本, 敦

× 橋本, 敦

WEKO 38013

ja 橋本, 敦

Search repository
HASHIMOTO, Atsushi

× HASHIMOTO, Atsushi

WEKO 38014

en HASHIMOTO, Atsushi

Search repository
八木, 直人

× 八木, 直人

WEKO 38015

ja 八木, 直人

Search repository
YAGI, Naoto

× YAGI, Naoto

WEKO 38016

en YAGI, Naoto

Search repository
中村, 佳朗

× 中村, 佳朗

WEKO 38017

ja 中村, 佳朗

Search repository
NAKAMURA, Yoshiaki

× NAKAMURA, Yoshiaki

WEKO 38018

en NAKAMURA, Yoshiaki

Search repository
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
キーワード
主題Scheme Other
主題 Panel Flutter
キーワード
主題Scheme Other
主題 Fluid-Structure Coupled Problem
キーワード
主題Scheme Other
主題 CFD-CSD Coupling
キーワード
主題Scheme Other
主題 Supersonic Boundary Layer
抄録
内容記述 A fluid-structure coupled computation code has been developed and applied to a panel flutter problem. The flutter velocities and the amplitudes of limit cycle oscillations obtained using the present method agree well with those of Dowell. It is found that the boundary layer over the panel can suppress flutter particularly in the Mach number region between 1.2 and 1.35, the effect of which increases with viscosity. In a 3D problem, good agreement was obtained between computation and experiment.
言語 en
内容記述タイプ Abstract
出版者
言語 ja
出版者 日本航空宇宙学会
言語
言語 jpn
資源タイプ
資源タイプresource http://purl.org/coar/resource_type/c_6501
タイプ journal article
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
ISSN
収録物識別子タイプ PISSN
収録物識別子 1344-6460
書誌情報 ja : 日本航空宇宙学会論文集

巻 55, 号 639, p. 159-164, 発行日 2007-04-05
フォーマット
application/pdf
著者版フラグ
値 publisher
URI
識別子 http://hdl.handle.net/2237/13877
識別子タイプ HDL
戻る
0
views
See details
Views

Versions

Ver.1 2021-03-01 19:04:37.294309
Show All versions

Share

Mendeley Twitter Facebook Print Addthis

Cite as

エクスポート

OAI-PMH
  • OAI-PMH JPCOAR
  • OAI-PMH DublinCore
  • OAI-PMH DDI
Other Formats
  • JSON
  • BIBTEX

Confirm


Powered by WEKO3


Powered by WEKO3