WEKO3
アイテム
{"_buckets": {"deposit": "73ae39e1-7e5c-4a37-8709-dc43a1411866"}, "_deposit": {"created_by": 1, "id": "45120", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "45120"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00045120", "sets": ["1893", "1917"]}, "author_link": ["473020", "473023", "473024", "473021", "473017", "473019", "473018", "473022"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Flow Quality of NAL Two-Dimensional Transonic Wind Tunnel Part IV Characteristics of Flow Control"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1985-06", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "63", "bibliographicVolumeNumber": "862", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-862", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The result of a flow control experiment conducted at the NAL blowdown type two-dimensional transonic wind tunnel are described in this report. This tunnel can be operated over a wide pressure range to change the test Reynolds number. The main features of the operation and control of this tunnel are the application of the precharged starting procedure for establishing high Reynolds number flow and the adoption of the closed-loop Mach number control which acts effectively in a short running time. It was found that high Reynolds number tests can be safely conducted and the flow duration can be increased by applying the precharged starting procedure. And also the closed-loop Mach number control showed excellent Mach numer repeatability within an error of ±0.001 at each run. An attempt to expand the operating envelope was successful with satisfying control accuracy.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR0862000", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: NAL TR-862", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory(NAL)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0389-4010", "subitem_source_identifier_type": "ISSN"}]}, "item_3_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: NAL-MATCH"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_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: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "三輪, 等"}], "nameIdentifiers": [{"nameIdentifier": "473017", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "佐藤, 衛"}], "nameIdentifiers": [{"nameIdentifier": "473018", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "小国, 保男"}], "nameIdentifiers": [{"nameIdentifier": "473019", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "神田, 宏"}], "nameIdentifiers": [{"nameIdentifier": "473020", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "MIWA, Hitoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473021", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "SATO, Mamoru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473022", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "OGUNI, Yasuo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473023", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "KANDA, Hiroshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "473024", "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": "2020-01-29"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltr00862.pdf", "filesize": [{"value": "4.1 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 4099999.9999999995, "url": {"label": "naltr00862.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/45120/files/naltr00862.pdf"}, "version_id": "9e199f58-692e-49da-8a37-7075760b98db"}]}, "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": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "航技研二次元風洞の気流特性について(Ⅳ)-二次元風洞気流制御-", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "航技研二次元風洞の気流特性について(Ⅳ)-二次元風洞気流制御-"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/45120", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "45120", "relation": {}, "relation_version_is_last": true, "title": ["航技研二次元風洞の気流特性について(Ⅳ)-二次元風洞気流制御-"], "weko_shared_id": -1}
航技研二次元風洞の気流特性について(Ⅳ)-二次元風洞気流制御-
https://jaxa.repo.nii.ac.jp/records/45120
https://jaxa.repo.nii.ac.jp/records/45120a875d8da-c48e-4906-88e2-016be2dae681
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr00862.pdf (4.1 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航技研二次元風洞の気流特性について(Ⅳ)-二次元風洞気流制御- | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Flow Quality of NAL Two-Dimensional Transonic Wind Tunnel Part IV Characteristics of Flow Control | |||||
著者 |
三輪, 等
× 三輪, 等× 佐藤, 衛× 小国, 保男× 神田, 宏× MIWA, Hitoshi× SATO, Mamoru× OGUNI, Yasuo× KANDA, Hiroshi |
|||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-862 巻 862, p. 63, 発行日 1985-06 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The result of a flow control experiment conducted at the NAL blowdown type two-dimensional transonic wind tunnel are described in this report. This tunnel can be operated over a wide pressure range to change the test Reynolds number. The main features of the operation and control of this tunnel are the application of the precharged starting procedure for establishing high Reynolds number flow and the adoption of the closed-loop Mach number control which acts effectively in a short running time. It was found that high Reynolds number tests can be safely conducted and the flow duration can be increased by applying the precharged starting procedure. And also the closed-loop Mach number control showed excellent Mach numer repeatability within an error of ±0.001 at each run. An attempt to expand the operating envelope was successful with satisfying control accuracy. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0862000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-862 |