WEKO3
アイテム
{"_buckets": {"deposit": "538edf2a-48b2-42f7-808d-6db105363b5c"}, "_deposit": {"created_by": 1, "id": "31590", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "31590"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00031590", "sets": ["1890", "1910"]}, "author_link": ["405078", "405082", "405079", "405081", "405077", "405080"], "item_9_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "An Experiment on Interaction of Shock Wave with Multiple-Orifice Plate by Means of Snap-Action Shock Tube"}]}, "item_9_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1976-01", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "4_B", "bibliographicPageEnd": "10", "bibliographicPageStart": "3", "bibliographicVolumeNumber": "11", "bibliographic_titles": [{"bibliographic_title": "東京大学宇宙航空研究所報告"}]}]}, "item_9_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper reports the performance and flow characteristics of the shock tube equipped ,with a shock wave valve, which is modified in more feasible fashion for practical use from one previously proposed by Muirhead et al. In order to clarify the starting processes of the multiple nozzles, an experiment was conducted by means of this shock tube to observe the feature of the flow accompanying with the shock waves reflected from and passing through the multiple-orifice plate set normal to the flow at the test section.", "subitem_description_type": "Other"}]}, "item_9_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: SA0124542000", "subitem_description_type": "Other"}]}, "item_9_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "東京大学宇宙航空研究所"}]}, "item_9_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0563-8100", "subitem_source_identifier_type": "ISSN"}]}, "item_9_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AN00161914", "subitem_source_identifier_type": "NCID"}]}, "item_9_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: ISASNII"}]}, "item_9_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 宇宙科学研究所"}]}, "item_9_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: 6"}]}, "item_9_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "小口, 伯郎"}], "nameIdentifiers": [{"nameIdentifier": "405077", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "船曳, 勝之"}], "nameIdentifiers": [{"nameIdentifier": "405078", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "佐藤, 俊逸"}], "nameIdentifiers": [{"nameIdentifier": "405079", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "OGUCHI, Hakuro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "405080", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "FUNABIKI, Katsushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "405081", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "SATO, Shunitsu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "405082", "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": "2020-01-23"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SA0124542.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": "SA0124542.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/31590/files/SA0124542.pdf"}, "version_id": "718f7e1c-6fa9-43c6-ac81-9d52312e3568"}]}, "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": "departmental bulletin paper", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験"}]}, "item_type_id": "9", "owner": "1", "path": ["1890", "1910"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/31590", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "31590", "relation": {}, "relation_version_is_last": true, "title": ["無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験"], "weko_shared_id": -1}
無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験
https://jaxa.repo.nii.ac.jp/records/31590
https://jaxa.repo.nii.ac.jp/records/3159025c55251-e019-4d8a-9a85-98cf97a0c0ec
名前 / ファイル | ライセンス | アクション |
---|---|---|
SA0124542.pdf (1.2 MB)
|
|
Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 無隔膜衝撃波管による多孔板と衝撃波の干渉に関する実験 | |||||
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_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | An Experiment on Interaction of Shock Wave with Multiple-Orifice Plate by Means of Snap-Action Shock Tube | |||||
著者 |
小口, 伯郎
× 小口, 伯郎× 船曳, 勝之× 佐藤, 俊逸× OGUCHI, Hakuro× FUNABIKI, Katsushi× SATO, Shunitsu |
|||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 11, 号 4_B, p. 3-10, 発行日 1976-01 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper reports the performance and flow characteristics of the shock tube equipped ,with a shock wave valve, which is modified in more feasible fashion for practical use from one previously proposed by Muirhead et al. In order to clarify the starting processes of the multiple nozzles, an experiment was conducted by means of this shock tube to observe the feature of the flow accompanying with the shock waves reflected from and passing through the multiple-orifice plate set normal to the flow at the test section. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0124542000 |