WEKO3
アイテム
{"_buckets": {"deposit": "c25acd91-1278-42c4-b91b-9197504bf456"}, "_deposit": {"created_by": 1, "id": "44743", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "44743"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00044743", "sets": ["1893", "1917"]}, "author_link": ["471018", "471016", "471015", "471017"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Experimental Investigation of the Effects of Side Jet on a Tail-fin of a Rocket in Supersonic Flow"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1977-02", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "30", "bibliographicVolumeNumber": "490", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-490", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "This paper describes the results of a test performed on the aerodynamic effects of a jet flow from the surface of a rocket on its tail-fin surface. In order to investigate these effects, pressure distribution on the tail-fin, pitot-pressure distribution and velocity vector distribution at the jet-core cross section were measured in a supersonic wind tunnel. Form the measured data, it was conclude that;1.The side jet ejected in the direction producing the pitch motion induces a pair of vortices at a point downstream from the jet nozzle, while the side jet ejected in the direction producing the roll motion induces only one large scale vortex. 2.In both cases, distorition of the pressure field on the tail-fin is due to the vortex or the vortices downstream of the jet nozzle.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR0490000", "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-490", "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"}]}, "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)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "外立, 政隆"}], "nameIdentifiers": [{"nameIdentifier": "471015", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "清水, 福壽"}], "nameIdentifiers": [{"nameIdentifier": "471016", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "HASHIDATE, Masataka", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "471017", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "SHIMIZU, Fukuji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "471018", "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": "naltr00490.pdf", "filesize": [{"value": "3.9 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 3900000.0, "url": {"label": "naltr00490.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/44743/files/naltr00490.pdf"}, "version_id": "993b2d0b-e4ae-4c72-a170-10615f3774a5"}]}, "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": "サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/44743", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "44743", "relation": {}, "relation_version_is_last": true, "title": ["サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験"], "weko_shared_id": -1}
サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験
https://jaxa.repo.nii.ac.jp/records/44743
https://jaxa.repo.nii.ac.jp/records/447433f4018fb-e1f1-44c6-a295-4da137bb72fb
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr00490.pdf (3.9 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 | サイド・ジェットのロケット尾翼におよぼす影響の超音速風胴実験 | |||||
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_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 | Experimental Investigation of the Effects of Side Jet on a Tail-fin of a Rocket in Supersonic Flow | |||||
著者 |
外立, 政隆
× 外立, 政隆× 清水, 福壽× HASHIDATE, Masataka× SHIMIZU, Fukuji |
|||||
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) | ||||||
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-490 巻 490, p. 30, 発行日 1977-02 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes the results of a test performed on the aerodynamic effects of a jet flow from the surface of a rocket on its tail-fin surface. In order to investigate these effects, pressure distribution on the tail-fin, pitot-pressure distribution and velocity vector distribution at the jet-core cross section were measured in a supersonic wind tunnel. Form the measured data, it was conclude that;1.The side jet ejected in the direction producing the pitch motion induces a pair of vortices at a point downstream from the jet nozzle, while the side jet ejected in the direction producing the roll motion induces only one large scale vortex. 2.In both cases, distorition of the pressure field on the tail-fin is due to the vortex or the vortices downstream of the jet nozzle. | |||||
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: NALTR0490000 | |||||
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-490 |