WEKO3
アイテム
{"_buckets": {"deposit": "19bf0a88-d75f-4fe6-b8e1-b7ee559a8957"}, "_deposit": {"created_by": 1, "id": "21665", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "21665"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00021665", "sets": ["1888"]}, "author_link": ["203305", "203302", "203306", "203304", "203303", "203307"], "item_7_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Performance Evaluation of Compression Ramp for Supersonic Intake in Propulsion/Airframe Integration Design"}]}, "item_7_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2015-12-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "6", "bibliographicPageEnd": "270(38)", "bibliographicPageStart": "265(33)", "bibliographicVolumeNumber": "63", "bibliographic_titles": [{"bibliographic_title": "日本航空宇宙学会論文集"}, {"bibliographic_title": "Journal of the Japan Society for Aeronautical and Space Sciences", "bibliographic_titleLang": "en"}]}]}, "item_7_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Diverter-less intake for supersonic aircraft is examined as a modern design technique of propulsion/airframe integration. In this study, a design guideline for the compression ramp in an external compression supersonic intake mounted on a low diverter or without diverter is examined by CFD analysis. We pursue the optimum configuration of the ramp which minimizes the boundary-layer flowing into intake without failing to decelerate the supersonic flow captured by an intake. The flow field over a single-stage rectangular wedge mounted on a flat surface was investigated under the free stream Mach number of 1.6. The results show that, under a given cross-sectional area of the intake throat, the width and angle of the ramp are important parameters to determine the optimum configuration. In order to decrease the mass flow rate of boundary-layer which flows into an intake, the ramp width should be small as long as the minimum decelerating demand is satisfied. The excessive large angle is not allowed because it induces substantial pressure loss of the main flow. In case of diverter-less configuration, the ramp width should be designed smaller than that in case of configuration with diverter to minimize the incoming boundary-layer.", "subitem_description_type": "Other"}]}, "item_7_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: 図版あり", "subitem_description_type": "Other"}]}, "item_7_description_19": {"attribute_name": "内容記述(英)", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains illustrations", "subitem_description_type": "Other"}]}, "item_7_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: DS1540389005", "subitem_description_type": "Other"}]}, "item_7_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "Japan Society for Aeronautical and Space Sciences"}]}, "item_7_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "日本航空宇宙学会"}]}, "item_7_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1344-6460", "subitem_source_identifier_type": "ISSN"}]}, "item_7_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11307372", "subitem_source_identifier_type": "NCID"}]}, "item_7_text_38": {"attribute_name": "NASA分類コード", "attribute_value_mlt": [{"subitem_text_value": "NASA分類コード: 02"}]}, "item_7_text_39": {"attribute_name": "NASA分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Aerodynamics"}]}, "item_7_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_access_right": {"attribute_name": "アクセス権", "attribute_value_mlt": [{"subitem_access_right": "metadata only access", "subitem_access_right_uri": "http://purl.org/coar/access_right/c_14cb"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "三木, 肇"}], "nameIdentifiers": [{"nameIdentifier": "203302", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "渡辺, 安"}], "nameIdentifiers": [{"nameIdentifier": "203303", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "亀田, 正治"}], "nameIdentifiers": [{"nameIdentifier": "203304", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Miki, Hajime", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "203305", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Watanabe, Yasushi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "203306", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kameda, Masaharu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "203307", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "Supersonic Intake", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Propulsion/Airframe Integration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Boundary-Layer", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "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": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "超音速機の機体/推進系統合設計におけるインテークランプの性能評価", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "超音速機の機体/推進系統合設計におけるインテークランプの性能評価"}]}, "item_type_id": "7", "owner": "1", "path": ["1888"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/21665", "pubdate": {"attribute_name": "公開日", "attribute_value": "2016-02-17"}, "publish_date": "2016-02-17", "publish_status": "0", "recid": "21665", "relation": {}, "relation_version_is_last": true, "title": ["超音速機の機体/推進系統合設計におけるインテークランプの性能評価"], "weko_shared_id": -1}
超音速機の機体/推進系統合設計におけるインテークランプの性能評価
https://jaxa.repo.nii.ac.jp/records/21665
https://jaxa.repo.nii.ac.jp/records/2166517584d6f-c174-4318-b07c-ffbee008b256
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-02-17 | |||||
タイトル | ||||||
タイトル | 超音速機の機体/推進系統合設計におけるインテークランプの性能評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Supersonic Intake | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Propulsion/Airframe Integration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Boundary-Layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
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 | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Performance Evaluation of Compression Ramp for Supersonic Intake in Propulsion/Airframe Integration Design | |||||
著者 |
三木, 肇
× 三木, 肇× 渡辺, 安× 亀田, 正治× Miki, Hajime× Watanabe, Yasushi× Kameda, Masaharu |
|||||
出版者 | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences | |||||
出版者(英) | ||||||
出版者 | 日本航空宇宙学会 | |||||
書誌情報 |
日本航空宇宙学会論文集 en : Journal of the Japan Society for Aeronautical and Space Sciences 巻 63, 号 6, p. 265(33)-270(38), 発行日 2015-12-05 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Diverter-less intake for supersonic aircraft is examined as a modern design technique of propulsion/airframe integration. In this study, a design guideline for the compression ramp in an external compression supersonic intake mounted on a low diverter or without diverter is examined by CFD analysis. We pursue the optimum configuration of the ramp which minimizes the boundary-layer flowing into intake without failing to decelerate the supersonic flow captured by an intake. The flow field over a single-stage rectangular wedge mounted on a flat surface was investigated under the free stream Mach number of 1.6. The results show that, under a given cross-sectional area of the intake throat, the width and angle of the ramp are important parameters to determine the optimum configuration. In order to decrease the mass flow rate of boundary-layer which flows into an intake, the ramp width should be small as long as the minimum decelerating demand is satisfied. The excessive large angle is not allowed because it induces substantial pressure loss of the main flow. In case of diverter-less configuration, the ramp width should be designed smaller than that in case of configuration with diverter to minimize the incoming boundary-layer. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 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 illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: DS1540389005 |