WEKO3
アイテム
{"_buckets": {"deposit": "34be28fe-4396-4e33-8242-f95f57a657c1"}, "_deposit": {"created_by": 1, "id": "5789", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "5789"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00005789", "sets": ["1005", "1891"]}, "author_link": ["477069", "477071", "477072", "477070"], "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2007-03-30", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "473", "bibliographicPageStart": "468", "bibliographicVolumeNumber": "JAXA-SP-06-029E", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料"}, {"bibliographic_title": "JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)", "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": "SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20011203-20011205 東京 日本", "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": "SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20011203-20011205 Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "CFD (Computational Fluid Dynamics) analyses of flow around NAL\u0027s non-powered supersonic experimental airplane are conducted. The results are compared with those of corresponding wind tunnel tests. In this paper, agreements and discrepancies between them are discussed in aspects of correspondence between calculation and test models.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0063609058", "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-06-029E", "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_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "航空力学"}, {"subitem_text_value": "数値解析"}, {"subitem_text_value": "航空機の設計、試験及び性能"}]}, "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_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_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": "三菱重工業"}, {"subitem_text_value": "三菱重工業"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Mitsubishi Heavy Industries Ltd."}, {"subitem_text_language": "en", "subitem_text_value": "Mitsubishi Heavy Industries Ltd."}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "吉本, 稔"}], "nameIdentifiers": [{"nameIdentifier": "477069", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "海田, 武司"}], "nameIdentifiers": [{"nameIdentifier": "477070", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yoshimoto, Minoru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "477071", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kaiden, Takeshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "477072", "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": "2020-02-10"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "63609058.pdf", "filesize": [{"value": "283.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 283900.0, "url": {"label": "63609058.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/5789/files/63609058.pdf"}, "version_id": "b6e86bb5-3cbf-4948-b2d0-4858d50582eb"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "超音速機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "航空機設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "流れの分布", "subitem_subject_scheme": "Other"}, {"subitem_subject": "計算流体力学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "実験機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "乱流", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax乱流モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "圧力分布", "subitem_subject_scheme": "Other"}, {"subitem_subject": "構造格子", "subitem_subject_scheme": "Other"}, {"subitem_subject": "超音速民間航空機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic aircraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aircraft design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flow distribution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational fluid dynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "research aircraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "turbulent flow", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Baldwin-Lomax turbulence model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "pressure distribution", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "structured grid", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic civil transport", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "Numerical simulations of flow around NAL\u0027s non-powered supersonic experimental airplane", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "Numerical simulations of flow around NAL\u0027s non-powered supersonic experimental airplane", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1005", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/5789", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "5789", "relation": {}, "relation_version_is_last": true, "title": ["Numerical simulations of flow around NAL\u0027s non-powered supersonic experimental airplane"], "weko_shared_id": -1}
Numerical simulations of flow around NAL's non-powered supersonic experimental airplane
https://jaxa.repo.nii.ac.jp/records/5789
https://jaxa.repo.nii.ac.jp/records/5789d0cb9ecb-bfda-4b10-a268-58696007ddb1
名前 / ファイル | ライセンス | アクション |
---|---|---|
63609058.pdf (283.9 kB)
|
|
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Numerical simulations of flow around NAL's non-powered supersonic experimental airplane | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れの分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 実験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Baldwin-Lomax乱流モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速民間航空機 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Baldwin-Lomax turbulence model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | structured grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic civil transport | |||||
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 | |||||
著者 |
吉本, 稔
× 吉本, 稔× 海田, 武司× Yoshimoto, Minoru× Kaiden, Takeshi |
|||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd. | ||||||
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 en : JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop) 巻 JAXA-SP-06-029E, p. 468-473, 発行日 2007-03-30 |
|||||
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 | SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20011203-20011205 東京 日本 | |||||
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 | SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20011203-20011205 Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | CFD (Computational Fluid Dynamics) analyses of flow around NAL's non-powered supersonic experimental airplane are conducted. The results are compared with those of corresponding wind tunnel tests. In this paper, agreements and discrepancies between them are discussed in aspects of correspondence between calculation and test models. | |||||
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: AA0063609058 | |||||
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-06-029E |