WEKO3
アイテム
{"_buckets": {"deposit": "3d45be22-4bbd-43f6-bd82-9f0a77140e7a"}, "_deposit": {"created_by": 1, "id": "4748", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "4748"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00004748", "sets": ["925", "1539", "1883", "1891"]}, "author_link": ["21595", "21597", "21592", "21590", "21594", "21596", "21593", "21591"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Sonic-boom analysis of a Concorde type airplane using the structured/unstructured overset grids method"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2011-02-28", "bibliographicIssueDateType": "Issued"}, "bibliographicVolumeNumber": "JAXA-SP-10-012", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010", "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42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP)", "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": "42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Sonic-boom due to a supersonic airplane is the one of the most serious problems to be solved for supersonic overland flight. Prediction of the sonic-boom on the ground is important to design a low-boom supersonic airplane. Structured/unstructured overset grids method is developed to estimate the ground the sonic-boom and evaluate the effects of the low-boom design concepts. The unstructured mesh CFD analysis solves only around the airplane. Then the structured mesh CFD analysis solves the near field pressure field using the results of unstructured mesh CFD analysis. The purpose of this overset grids method is to predict the near-field pressure signatures accurately and efficiently which are used to estimate the sonic-boom on the ground. In this paper, the structured/unstructured overset grids method is applied to the Darden\u0027s low-boom axisymmetric shape and Concorde type airplane.", "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: AA0064967041", "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-10-012", "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"}]}, "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_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_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: 7"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "三向ソフトウェア開発"}, {"subitem_text_value": "宇宙航空研究開発機構"}, {"subitem_text_value": "宇宙航空研究開発機構"}, {"subitem_text_value": "菱友システムズ"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Sanko Soft"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency (JAXA)"}, {"subitem_text_language": "en", "subitem_text_value": "Ryoyu Systems"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "石川, 敬掲"}], "nameIdentifiers": [{"nameIdentifier": "21590", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "牧野, 好和"}], "nameIdentifiers": [{"nameIdentifier": "21591", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "吉田, 憲司"}], "nameIdentifiers": [{"nameIdentifier": "21592", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "大平, 啓介"}], "nameIdentifiers": [{"nameIdentifier": "21593", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ishikawa, Hiroaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "21594", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Makino, Yoshikazu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "21595", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yoshida, Kenji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "21596", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ohira, Keisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "21597", "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": "64967041.pdf", "filesize": [{"value": "1.6 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1600000.0, "url": {"label": "64967041.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/4748/files/64967041.pdf"}, "version_id": "973a3fa1-00ec-454f-b7a5-027c6468035e"}]}, "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": "構造/非構造重合格子法を用いたコンコルド模擬形状のソニックブーム解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "構造/非構造重合格子法を用いたコンコルド模擬形状のソニックブーム解析"}]}, "item_type_id": "5", "owner": "1", "path": ["925", "1539", "1883", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/4748", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "4748", "relation": {}, "relation_version_is_last": true, "title": ["構造/非構造重合格子法を用いたコンコルド模擬形状のソニックブーム解析"], "weko_shared_id": -1}
構造/非構造重合格子法を用いたコンコルド模擬形状のソニックブーム解析
https://jaxa.repo.nii.ac.jp/records/4748
https://jaxa.repo.nii.ac.jp/records/47483a3e91ca-f356-43be-b890-83d518f9de72
名前 / ファイル | ライセンス | アクション |
---|---|---|
64967041.pdf (1.6 MB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 構造/非構造重合格子法を用いたコンコルド模擬形状のソニックブーム解析 | |||||
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 | Sonic-boom analysis of a Concorde type airplane using the structured/unstructured overset grids method | |||||
著者 |
石川, 敬掲
× 石川, 敬掲× 牧野, 好和× 吉田, 憲司× 大平, 啓介× Ishikawa, Hiroaki× Makino, Yoshikazu× Yoshida, Kenji× Ohira, Keisuke |
|||||
著者所属 | ||||||
三向ソフトウェア開発 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Sanko Soft | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
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42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集 en : JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 巻 JAXA-SP-10-012, 発行日 2011-02-28 |
|||||
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42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP) | |||||
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 | 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Sonic-boom due to a supersonic airplane is the one of the most serious problems to be solved for supersonic overland flight. Prediction of the sonic-boom on the ground is important to design a low-boom supersonic airplane. Structured/unstructured overset grids method is developed to estimate the ground the sonic-boom and evaluate the effects of the low-boom design concepts. The unstructured mesh CFD analysis solves only around the airplane. Then the structured mesh CFD analysis solves the near field pressure field using the results of unstructured mesh CFD analysis. The purpose of this overset grids method is to predict the near-field pressure signatures accurately and efficiently which are used to estimate the sonic-boom on the ground. In this paper, the structured/unstructured overset grids method is applied to the Darden's low-boom axisymmetric shape and Concorde type airplane. | |||||
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: AA0064967041 | |||||
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-10-012 |