WEKO3
アイテム
{"_buckets": {"deposit": "20e45d92-112d-473c-baa7-4e83cc109d0b"}, "_deposit": {"created_by": 1, "id": "3860", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "3860"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00003860", "sets": ["859", "1535", "1879", "1891"]}, "author_link": ["16298", "16296", "16297", "16299", "16295", "16294"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Highly-accurate Computation of Supersonic Flows around a Concave Body"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2015-03-25", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "144", "bibliographicPageStart": "139", "bibliographicVolumeNumber": "JAXA-SP-14-010", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium", "bibliographic_titleLang": "en"}]}]}, "item_5_description_14": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)", "attribute_value_mlt": [{"subitem_description": "第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県", "subitem_description_type": "Other"}]}, "item_5_description_15": {"attribute_name": "会議概要(会議名, 開催地, 会期, 主催者等)(英)", "attribute_value_mlt": [{"subitem_description": "46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The supersonic parachute has been used to many space probes for aerodynamic deceleration at the time of the atmospheric re-entry. However, its detailed aerodynamic characteristics have not been made clear. The purpose of this study is to investigate basic flow phenomena and aerodynamic characteristics on a rectangular concave body in supersonic flows by means of high-resolutional numerical computations using the WENO scheme. As results, the following characteristics have been captured: 1) in the case of quasi-stationary flows, vortices are shed from the detached bow shock wave, and especially in mean stream Mach number greater than three the vortices are to flow toward the inner portion of the concave body; 2) in time history of lift coefficients, peaks of low and high frequencies are observed in the FFT analysis, and the former and the latter oscillations are due to the outer and inner regions of the body, respectively; 3) in the transient cases when disturbances are given, pressure waves go and return in the space between the detached shock wave and the concave bottom, and vortices are shed from the center portion of the shock wave, with movements of shock location.", "subitem_description_type": "Other"}]}, "item_5_description_18": {"attribute_name": "内容記述", "attribute_value_mlt": [{"subitem_description": "形態: カラー図版あり", "subitem_description_type": "Other"}]}, "item_5_description_19": {"attribute_name": "内容記述(英)", "attribute_value_mlt": [{"subitem_description": "Physical characteristics: Original contains color illustrations", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA1530023025", "subitem_description_type": "Other"}]}, "item_5_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: JAXA-SP-14-010", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構(JAXA)"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "subitem_source_identifier_type": "ISSN"}]}, "item_5_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11984031", "subitem_source_identifier_type": "NCID"}]}, "item_5_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: JAXA"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 特別資料"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_5_text_38": {"attribute_name": "NASA分類コード", "attribute_value_mlt": [{"subitem_text_value": "NASA分類コード: 34"}]}, "item_5_text_39": {"attribute_name": "NASA分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Fluid Mechanics and Thermodynamics"}]}, "item_5_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "item_5_text_41": {"attribute_name": "jaxa出版物シリーズ", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物シリーズ: 015"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 521"}]}, "item_5_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_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東海大学"}, {"subitem_text_value": "東海大学"}, {"subitem_text_value": "東海大学"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Tokai University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokai University"}, {"subitem_text_language": "en", "subitem_text_value": "Tokai University"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "尾崎, 彰彦"}], "nameIdentifiers": [{"nameIdentifier": "16294", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "豊里, 理紗"}], "nameIdentifiers": [{"nameIdentifier": "16295", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "高倉, 葉子"}], "nameIdentifiers": [{"nameIdentifier": "16296", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ozaki, Akihiko", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "16297", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Toyosato, Risa", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "16298", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takakura, Yoko", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "16299", "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": "2020-01-16"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "AA1530023025.pdf", "filesize": [{"value": "1.4 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1400000.0, "url": {"label": "AA1530023025.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/3860/files/AA1530023025.pdf"}, "version_id": "f6892a18-6860-4837-bca1-d260074dce07"}]}, "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "超音速流中における凹状物体まわりの流れの高精度数値計算", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "超音速流中における凹状物体まわりの流れの高精度数値計算"}]}, "item_type_id": "5", "owner": "1", "path": ["859", "1535", "1879", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/3860", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-05-08"}, "publish_date": "2015-05-08", "publish_status": "0", "recid": "3860", "relation": {}, "relation_version_is_last": true, "title": ["超音速流中における凹状物体まわりの流れの高精度数値計算"], "weko_shared_id": -1}
超音速流中における凹状物体まわりの流れの高精度数値計算
https://jaxa.repo.nii.ac.jp/records/3860
https://jaxa.repo.nii.ac.jp/records/3860147e1adf-48b0-423e-9ebb-8fad370c4153
名前 / ファイル | ライセンス | アクション |
---|---|---|
AA1530023025.pdf (1.4 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-05-08 | |||||
タイトル | ||||||
タイトル | 超音速流中における凹状物体まわりの流れの高精度数値計算 | |||||
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_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Highly-accurate Computation of Supersonic Flows around a Concave Body | |||||
著者 |
尾崎, 彰彦
× 尾崎, 彰彦× 豊里, 理紗× 高倉, 葉子× Ozaki, Akihiko× Toyosato, Risa× Takakura, Yoko |
|||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-14-010, p. 139-144, 発行日 2015-03-25 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The supersonic parachute has been used to many space probes for aerodynamic deceleration at the time of the atmospheric re-entry. However, its detailed aerodynamic characteristics have not been made clear. The purpose of this study is to investigate basic flow phenomena and aerodynamic characteristics on a rectangular concave body in supersonic flows by means of high-resolutional numerical computations using the WENO scheme. As results, the following characteristics have been captured: 1) in the case of quasi-stationary flows, vortices are shed from the detached bow shock wave, and especially in mean stream Mach number greater than three the vortices are to flow toward the inner portion of the concave body; 2) in time history of lift coefficients, peaks of low and high frequencies are observed in the FFT analysis, and the former and the latter oscillations are due to the outer and inner regions of the body, respectively; 3) in the transient cases when disturbances are given, pressure waves go and return in the space between the detached shock wave and the concave bottom, and vortices are shed from the center portion of the shock wave, with movements of shock location. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1530023025 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-14-010 |