WEKO3
アイテム
{"_buckets": {"deposit": "67ee5e7a-5059-4756-856c-b8ed2a4eb178"}, "_deposit": {"created_by": 1, "id": "6595", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6595"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006595", "sets": ["1365", "1891"]}, "author_link": ["33748", "33752", "33750", "33751", "33754", "33753", "33749", "33755"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Wind tunnel test using scaled model rotor system"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-03-25", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "50", "bibliographicPageStart": "44", "bibliographicVolumeNumber": "JAXA-SP-03-003", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第66回 風洞研究会議論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper presents the outline of the scaled model rotor system, which was used in 2 m by 2 m FHI low-speed wind tunnel, and some typical wind tunnel tests. The scaled model rotor system has been applied for many fundamental tests and development tests since 1991. The system consists of teetering type hub, blades, pylon, rotary balance and servomotor etc. The collective pitch and cyclic pitch can be changed with remote control.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047428006", "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-03-003", "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"}]}, "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": "富士重工業"}, {"subitem_text_value": "富士重工業"}, {"subitem_text_value": "富士重工業"}, {"subitem_text_value": "富士重工業"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Fuji Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Fuji Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Fuji Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Fuji Heavy Industries Ltd."}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "塚原, 孝則"}], "nameIdentifiers": [{"nameIdentifier": "33748", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "橋口, 祐子"}], "nameIdentifiers": [{"nameIdentifier": "33749", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "太田, 智基"}], "nameIdentifiers": [{"nameIdentifier": "33750", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小生方, 正裕"}], "nameIdentifiers": [{"nameIdentifier": "33751", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tsukahara, Takanori", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "33752", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Hashiguchi, Yuko", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "33753", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ota, Tomoki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "33754", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Obukata, Masahiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "33755", "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": "47428006.pdf", "filesize": [{"value": "1.7 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1700000.0, "url": {"label": "47428006.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6595/files/47428006.pdf"}, "version_id": "e431911d-2050-46c7-b657-ff3197002138"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "ヘリコプタ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞模型", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ロータダイナミクス", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ロータブレード", "subitem_subject_scheme": "Other"}, {"subitem_subject": "騒音低減", "subitem_subject_scheme": "Other"}, {"subitem_subject": "振動減衰", "subitem_subject_scheme": "Other"}, {"subitem_subject": "低層音翼端", "subitem_subject_scheme": "Other"}, {"subitem_subject": "helicopter", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rotor dynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rotor blade", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "noise reduction", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "vibration damping", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "low noise wing tip", "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": "ロータ模型回転装置を用いた風洞試験", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "ロータ模型回転装置を用いた風洞試験"}]}, "item_type_id": "5", "owner": "1", "path": ["1365", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6595", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6595", "relation": {}, "relation_version_is_last": true, "title": ["ロータ模型回転装置を用いた風洞試験"], "weko_shared_id": -1}
ロータ模型回転装置を用いた風洞試験
https://jaxa.repo.nii.ac.jp/records/6595
https://jaxa.repo.nii.ac.jp/records/65950e2e342e-29ba-492f-8531-299b06c59168
名前 / ファイル | ライセンス | アクション |
---|---|---|
47428006.pdf (1.7 MB)
|
|
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 | ロータ模型回転装置を用いた風洞試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘリコプタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロータダイナミクス | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロータブレード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 騒音低減 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動減衰 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低層音翼端 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | helicopter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rotor blade | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | noise reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vibration damping | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low noise wing tip | |||||
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 | Wind tunnel test using scaled model rotor system | |||||
著者 |
塚原, 孝則
× 塚原, 孝則× 橋口, 祐子× 太田, 智基× 小生方, 正裕× Tsukahara, Takanori× Hashiguchi, Yuko× Ota, Tomoki× Obukata, Masahiro |
|||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属 | ||||||
富士重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Heavy Industries Ltd. | ||||||
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: 第66回 風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting 巻 JAXA-SP-03-003, p. 44-50, 発行日 2004-03-25 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents the outline of the scaled model rotor system, which was used in 2 m by 2 m FHI low-speed wind tunnel, and some typical wind tunnel tests. The scaled model rotor system has been applied for many fundamental tests and development tests since 1991. The system consists of teetering type hub, blades, pylon, rotary balance and servomotor etc. The collective pitch and cyclic pitch can be changed with remote control. | |||||
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: AA0047428006 | |||||
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-03-003 |