WEKO3
アイテム
{"_buckets": {"deposit": "189abe95-8b17-43ba-b046-145ebfbb1e6a"}, "_deposit": {"created_by": 1, "id": "33246", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "33246"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00033246", "sets": ["1890", "1991"]}, "author_link": ["415776", "415775"], "item_9_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2003-03", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "132", "bibliographicPageStart": "123", "bibliographicVolumeNumber": "17", "bibliographic_titles": [{}, {"bibliographic_title": "The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule", "bibliographic_titleLang": "en"}]}]}, "item_9_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Effect of earlier turbulent transition and enhancement of turbulence intensity in the boundary layer due to ablation product gas is discussed in terms of anomalous heating profile over the surface of an entry capsule. First, a numerical approach that utilizes Park\u0027s injection induced turbulence model is described and some of the numerical results for code validation study are shown. Second, calculated results of trajectory-based aerodynamic heating environment for Pioneer-Venus entry capsules are shown. Finally, a numerical prediction of trajectory-based aerodynamic heating environment for MUSES-C is made and the possible effect of earlier turbulent transition is discussed.", "subitem_description_type": "Other"}]}, "item_9_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: SA0200019000", "subitem_description_type": "Other"}]}, "item_9_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙科学研究所"}]}, "item_9_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Institute of Space and Astronautical Science"}]}, "item_9_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0288-433X", "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": "AA10455137", "subitem_source_identifier_type": "NCID"}]}, "item_9_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "宇宙科学研究"}, {"subitem_text_value": "宇宙工学"}, {"subitem_text_value": "人工衛星・探査機"}, {"subitem_text_value": "小惑星探査機「はやぶさ(MUSES-C)」"}]}, "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": "東北大学大学院 工学研究科 航空宇宙工学専攻"}]}, "item_9_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Department of Aeronautics and Space Engineering, Tohoku University"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "澤田, 恵介"}], "nameIdentifiers": [{"nameIdentifier": "415775", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sawada, Keisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "415776", "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": "2020-01-24"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SA0200019.pdf", "filesize": [{"value": "2.8 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 2800000.0, "url": {"label": "SA0200019.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/33246/files/SA0200019.pdf"}, "version_id": "8355b0fe-8e86-4deb-bc03-5801c31bafdd"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "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": "Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition", "subitem_title_language": "en"}]}, "item_type_id": "9", "owner": "1", "path": ["1890", "1991"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/33246", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "33246", "relation": {}, "relation_version_is_last": true, "title": ["Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition"], "weko_shared_id": -1}
Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition
https://jaxa.repo.nii.ac.jp/records/33246
https://jaxa.repo.nii.ac.jp/records/3324657f15b1f-e152-440a-9414-536f1e50069b
名前 / ファイル | ライセンス | アクション |
---|---|---|
SA0200019.pdf (2.8 MB)
|
|
Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Anomalous Heating Profile over Entry Capsule with Ablation and Its Relation to Earlier Turbulent Transition | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
著者 |
澤田, 恵介
× 澤田, 恵介× Sawada, Keisuke |
|||||
著者所属 | ||||||
東北大学大学院 工学研究科 航空宇宙工学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautics and Space Engineering, Tohoku University | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule 巻 17, p. 123-132, 発行日 2003-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Effect of earlier turbulent transition and enhancement of turbulence intensity in the boundary layer due to ablation product gas is discussed in terms of anomalous heating profile over the surface of an entry capsule. First, a numerical approach that utilizes Park's injection induced turbulence model is described and some of the numerical results for code validation study are shown. Second, calculated results of trajectory-based aerodynamic heating environment for Pioneer-Venus entry capsules are shown. Finally, a numerical prediction of trajectory-based aerodynamic heating environment for MUSES-C is made and the possible effect of earlier turbulent transition is discussed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0288-433X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10455137 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0200019000 |