WEKO3
アイテム
{"_buckets": {"deposit": "8b581046-7386-48aa-a5a1-05f373072b6a"}, "_deposit": {"created_by": 1, "id": "2936", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "2936"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00002936", "sets": ["1531", "1875", "1891", "1976"]}, "author_link": ["9976", "9977", "9978", "9979", "9975", "9980"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Preliminary Experiment on Hypersonic Boundary Layer Flow Control using Discharge Chamber under Body Surface"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2019-02-25", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "106", "bibliographicPageStart": "103", "bibliographicVolumeNumber": "JAXA-SP-18-005", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36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 50th Fluid Dynamics Conference / the 36th 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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎", "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": "50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen\u0027s Plaza), Miyazaki, Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In recent years, the flow control method using plasma discharge, for example, a plasma actuator, has been attracting attention, because of its shorter response-time than conventional mechanical control devices such as flaps. In this study, a flat plate model with a small cavity under the surface was tested for the discharge experiment in the Mach 7 hypersonic wind tunnel in Kashiwa campus, the University of Tokyo. Two types of the discharge cavities were tested: a cavity with an orifice normal to the surface and a cavity with an orifice and a forward-facing-step inlet open to the boundary layer flow. A pair of tungsten rod-type electrodes were inserted into the cavity, and the applied voltage was 1kV at maximum using high-power capacitors. The discharge occurred intermittently and the time history of the discharge voltage was measured. The effect of the discharge on the flow field was visualized by the schlieren method. In the case of the intake moved slightly forward when the discharge occurred.", "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: AA1830029007", "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-18-005", "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: 75"}]}, "item_5_text_39": {"attribute_name": "NASA分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Plasma Physics"}]}, "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": "東京大学"}, {"subitem_text_value": "東京大学"}, {"subitem_text_value": "東京大学"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "The University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "The University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "The University of Tokyo"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "森, 直紀"}], "nameIdentifiers": [{"nameIdentifier": "9975", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "渡邉, 保真"}], "nameIdentifiers": [{"nameIdentifier": "9976", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "鈴木, 宏二郎"}], "nameIdentifiers": [{"nameIdentifier": "9977", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Mori, Naoki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "9978", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Watanabe, Yasumasa", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "9979", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Suzuki, Kojiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "9980", "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": "AA1830029007.pdf", "filesize": [{"value": "5.5 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 5500000.0, "url": {"label": "AA1830029007.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/2936/files/AA1830029007.pdf"}, "version_id": "8476b063-d5f3-46e1-98d6-741e5b909b5b"}]}, "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": "模型表面内側に設けた放電室による極超音速境界層流れ制御の基礎実験", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "模型表面内側に設けた放電室による極超音速境界層流れ制御の基礎実験"}]}, "item_type_id": "5", "owner": "1", "path": ["1531", "1875", "1891", "1976"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/2936", "pubdate": {"attribute_name": "公開日", "attribute_value": "2019-02-28"}, "publish_date": "2019-02-28", "publish_status": "0", "recid": "2936", "relation": {}, "relation_version_is_last": true, "title": ["模型表面内側に設けた放電室による極超音速境界層流れ制御の基礎実験"], "weko_shared_id": -1}
模型表面内側に設けた放電室による極超音速境界層流れ制御の基礎実験
https://jaxa.repo.nii.ac.jp/records/2936
https://jaxa.repo.nii.ac.jp/records/2936a362e956-6886-4bcc-ad8b-521bd6cf06ec
名前 / ファイル | ライセンス | アクション |
---|---|---|
AA1830029007.pdf (5.5 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | 模型表面内側に設けた放電室による極超音速境界層流れ制御の基礎実験 | |||||
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 | Preliminary Experiment on Hypersonic Boundary Layer Flow Control using Discharge Chamber under Body Surface | |||||
著者 |
森, 直紀
× 森, 直紀× 渡邉, 保真× 鈴木, 宏二郎× Mori, Naoki× Watanabe, Yasumasa× Suzuki, Kojiro |
|||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
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50回流体力学講演会/第36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 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-18-005, p. 103-106, 発行日 2019-02-25 |
|||||
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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎 | |||||
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 | 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In recent years, the flow control method using plasma discharge, for example, a plasma actuator, has been attracting attention, because of its shorter response-time than conventional mechanical control devices such as flaps. In this study, a flat plate model with a small cavity under the surface was tested for the discharge experiment in the Mach 7 hypersonic wind tunnel in Kashiwa campus, the University of Tokyo. Two types of the discharge cavities were tested: a cavity with an orifice normal to the surface and a cavity with an orifice and a forward-facing-step inlet open to the boundary layer flow. A pair of tungsten rod-type electrodes were inserted into the cavity, and the applied voltage was 1kV at maximum using high-power capacitors. The discharge occurred intermittently and the time history of the discharge voltage was measured. The effect of the discharge on the flow field was visualized by the schlieren method. In the case of the intake moved slightly forward when the discharge occurred. | |||||
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: AA1830029007 | |||||
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-18-005 |