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": "3df0ce11-eddd-48a4-951c-7b0fc6410ad4"}, "_deposit": {"id": "12060", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "12060"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00012060", "sets": ["322"]}, "author_link": ["38248", "38249", "38250", "38251", "38252", "38253", "38254", "38255", "38256", "38257"], "item_10_alternative_title_19": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "Flutter Analysis of a Curved PanelUsing a Fluid-Structure Coupled Scheme", "subitem_alternative_title_language": "en"}]}, "item_10_biblio_info_6": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2007", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "638", "bibliographicPageEnd": "155", "bibliographicPageStart": "150", "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 computational program using a CFD-CSD coupled method has been developed to study the problem of low supersonic curved panel flutter. So far the supersonic aerodynamic model has been commonly employed to compute flutter boundaries. However, the present CFD-CSD coupled method makes it possible to analyze flutter boundaries at all speeds including transonic speeds. The computed flutter dynamic pressure for M∞=3 agrees with others’ results. A curved panel flutter were analyzed at a low supersonic speed, M∞=1.2. The flutter for small curvature panels is first-mode flutter, which is similar to flat panel flutter, whereas it becomes higher-mode flutter for larger curvature plates. In this study, flutter boundaries for an access panel have also been simulated. Its critical dynamic pressure becomes significantly lower compared with the case of a panel with its all edges simply supported.", "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/2237/13938"}]}, "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": "38248", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hashimoto, Atsushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38249", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "八木, 直人", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38250", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yagi, Naoto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38251", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中村, 佳朗", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38252", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakamura, Yoshiaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38253", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "伊藤, 文博", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38254", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ito, Fumihiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38255", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "海田, 武司", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "38256", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kaiden, Takeshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "38257", "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_n638.pdf", "filesize": [{"value": "1.0 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_note", "mimetype": "application/pdf", "size": 1000000.0, "url": {"label": "jjsass_v55_n638.pdf", "objectType": "fulltext", "url": "https://nagoya.repo.nii.ac.jp/record/12060/files/jjsass_v55_n638.pdf"}, "version_id": "74a9e722-6821-4b1a-9a50-daa0f9ef0016"}]}, "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": "曲面パネルの流体構造連成計算法によるフラッタ解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "曲面パネルの流体構造連成計算法によるフラッタ解析", "subitem_title_language": "ja"}]}, "item_type_id": "10", "owner": "1", "path": ["322"], "permalink_uri": "http://hdl.handle.net/2237/13938", "pubdate": {"attribute_name": "PubDate", "attribute_value": "2010-08-03"}, "publish_date": "2010-08-03", "publish_status": "0", "recid": "12060", "relation": {}, "relation_version_is_last": true, "title": ["曲面パネルの流体構造連成計算法によるフラッタ解析"], "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

曲面パネルの流体構造連成計算法によるフラッタ解析

http://hdl.handle.net/2237/13938
http://hdl.handle.net/2237/13938
9a1c7ce7-d7a6-44a5-b9be-21b31d9dca77
名前 / ファイル ライセンス アクション
jjsass_v55_n638.pdf jjsass_v55_n638.pdf (1.0 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2010-08-03
タイトル
タイトル 曲面パネルの流体構造連成計算法によるフラッタ解析
言語 ja
その他のタイトル
その他のタイトル Flutter Analysis of a Curved PanelUsing a Fluid-Structure Coupled Scheme
言語 en
著者 橋本, 敦

× 橋本, 敦

WEKO 38248

ja 橋本, 敦

Search repository
Hashimoto, Atsushi

× Hashimoto, Atsushi

WEKO 38249

en Hashimoto, Atsushi

Search repository
八木, 直人

× 八木, 直人

WEKO 38250

ja 八木, 直人

Search repository
Yagi, Naoto

× Yagi, Naoto

WEKO 38251

en Yagi, Naoto

Search repository
中村, 佳朗

× 中村, 佳朗

WEKO 38252

ja 中村, 佳朗

Search repository
Nakamura, Yoshiaki

× Nakamura, Yoshiaki

WEKO 38253

en Nakamura, Yoshiaki

Search repository
伊藤, 文博

× 伊藤, 文博

WEKO 38254

ja 伊藤, 文博

Search repository
Ito, Fumihiro

× Ito, Fumihiro

WEKO 38255

en Ito, Fumihiro

Search repository
海田, 武司

× 海田, 武司

WEKO 38256

ja 海田, 武司

Search repository
Kaiden, Takeshi

× Kaiden, Takeshi

WEKO 38257

en Kaiden, Takeshi

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
抄録
内容記述 A computational program using a CFD-CSD coupled method has been developed to study the problem of low supersonic curved panel flutter. So far the supersonic aerodynamic model has been commonly employed to compute flutter boundaries. However, the present CFD-CSD coupled method makes it possible to analyze flutter boundaries at all speeds including transonic speeds. The computed flutter dynamic pressure for M∞=3 agrees with others’ results. A curved panel flutter were analyzed at a low supersonic speed, M∞=1.2. The flutter for small curvature panels is first-mode flutter, which is similar to flat panel flutter, whereas it becomes higher-mode flutter for larger curvature plates. In this study, flutter boundaries for an access panel have also been simulated. Its critical dynamic pressure becomes significantly lower compared with the case of a panel with its all edges simply supported.
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 638, p. 150-155, 発行日 2007
フォーマット
application/pdf
著者版フラグ
値 publisher
URI
識別子 http://hdl.handle.net/2237/13938
識別子タイプ HDL
戻る
0
views
See details
Views

Versions

Ver.1 2021-03-01 19:02:57.474414
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