WEKO3
アイテム
{"_buckets": {"deposit": "2e88b0de-3975-4993-8715-c7421f8929a1"}, "_deposit": {"created_by": 1, "id": "3245", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "3245"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00003245", "sets": ["1532", "1876", "1891", "1978"]}, "author_link": ["12482", "12479", "12483", "12480", "12484", "12481"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Development of Magnetic Suspension and Balance System for High Subsonic Wind Tunnel"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2017-12-27", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "88", "bibliographicPageStart": "83", "bibliographicVolumeNumber": "JAXA-SP-17-004", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium", "bibliographic_titleLang": "en"}]}]}, "item_5_description_14": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)", "attribute_value_mlt": [{"subitem_description": "第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-41日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京", "subitem_description_type": "Other"}]}, "item_5_description_15": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)(英)", "attribute_value_mlt": [{"subitem_description": "49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The magnetic suspension and balance system (MSBS) suspending the model against high subsonic flow has been successfully developed at Japan Aerospace Exploration Agency (JAXA). In transonic regime, there are difficulties for MSBS to support the model because aerodynamic force acting on the model increases and its fluctuation also increases accordingly. One of JAXA\u0027s MSBS for the 10 cm low speed wind tunnel was modified to improve control system response. A 500 Hz control system with image sensors was developed, and the proportional-integral controller was replaced to proportional-integral-differential controller. In addition, to cope with the larger aerodynamic force, more powerful amplifiers were installed and stronger magnets were also installed in the model. The improved MSBS suspended an ogive-cylinder model with diameter of 10 mm and length of 156 mm up to Mach number of 0.6.", "subitem_description_type": "Other"}]}, "item_5_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_5_description_19": {"attribute_name": "内容記述(英)", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains color illustrations", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA1730011011", "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-17-004", "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(JAXA)"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_5_source_id_22": {"attribute_name": "ISSNONLINE", "attribute_value_mlt": [{"subitem_source_identifier": "2433-2232", "subitem_source_identifier_type": "ISSN"}]}, "item_5_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: JAXA"}]}, "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_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_5_text_38": {"attribute_name": "NASA分類コード", "attribute_value_mlt": [{"subitem_text_value": "NASA分類コード: 09"}]}, "item_5_text_39": {"attribute_name": "NASA分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Research and Support Facilities (Air)"}]}, "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_41": {"attribute_name": "jaxa出版物シリーズ", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物シリーズ: 015"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 521"}]}, "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: 10"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "早稲田大学"}, {"subitem_text_value": "宇宙航空研究開発機構(JAXA)"}, {"subitem_text_value": "早稲田大学"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Waseda University"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Waseda University"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "甲斐, 大貴"}], "nameIdentifiers": [{"nameIdentifier": "12479", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "杉浦, 裕樹"}], "nameIdentifiers": [{"nameIdentifier": "12480", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "手塚, 亜聖"}], "nameIdentifiers": [{"nameIdentifier": "12481", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kai, Daiki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "12482", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sugiura, Hiroki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "12483", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tezuka, Asei", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "12484", "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": "2020-01-15"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "AA1730011011.pdf", "filesize": [{"value": "1.2 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1200000.0, "url": {"label": "AA1730011011.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/3245/files/AA1730011011.pdf"}, "version_id": "3e984a94-b45c-40ea-8524-e4487c5b29d9"}]}, "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": "高亜音速磁力支持天秤風洞の開発", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "高亜音速磁力支持天秤風洞の開発"}]}, "item_type_id": "5", "owner": "1", "path": ["1532", "1876", "1891", "1978"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/3245", "pubdate": {"attribute_name": "公開日", "attribute_value": "2017-12-28"}, "publish_date": "2017-12-28", "publish_status": "0", "recid": "3245", "relation": {}, "relation_version_is_last": true, "title": ["高亜音速磁力支持天秤風洞の開発"], "weko_shared_id": -1}
高亜音速磁力支持天秤風洞の開発
https://jaxa.repo.nii.ac.jp/records/3245
https://jaxa.repo.nii.ac.jp/records/3245c32d7b40-f7dc-46d1-9ddf-2dd2f65abe69
名前 / ファイル | ライセンス | アクション |
---|---|---|
AA1730011011.pdf (1.2 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2017-12-28 | |||||
タイトル | ||||||
タイトル | 高亜音速磁力支持天秤風洞の開発 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Development of Magnetic Suspension and Balance System for High Subsonic Wind Tunnel | |||||
著者 |
甲斐, 大貴
× 甲斐, 大貴× 杉浦, 裕樹× 手塚, 亜聖× Kai, Daiki× Sugiura, Hiroki× Tezuka, Asei |
|||||
著者所属 | ||||||
早稲田大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
早稲田大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Waseda University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Waseda University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-17-004, p. 83-88, 発行日 2017-12-27 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-41日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The magnetic suspension and balance system (MSBS) suspending the model against high subsonic flow has been successfully developed at Japan Aerospace Exploration Agency (JAXA). In transonic regime, there are difficulties for MSBS to support the model because aerodynamic force acting on the model increases and its fluctuation also increases accordingly. One of JAXA's MSBS for the 10 cm low speed wind tunnel was modified to improve control system response. A 500 Hz control system with image sensors was developed, and the proportional-integral controller was replaced to proportional-integral-differential controller. In addition, to cope with the larger aerodynamic force, more powerful amplifiers were installed and stronger magnets were also installed in the model. The improved MSBS suspended an ogive-cylinder model with diameter of 10 mm and length of 156 mm up to Mach number of 0.6. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1730011011 | |||||
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-17-004 |