WEKO3
アイテム
{"_buckets": {"deposit": "f58d1a5c-c538-4026-911a-a830a822b967"}, "_deposit": {"created_by": 1, "id": "37405", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "37405"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00037405", "sets": ["1891", "1915"]}, "author_link": ["480609", "480615", "480611", "480614", "480613", "480610", "480608", "480612"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Natural laminar flow wing design of NAL\u0027s scaled supersonic experimental airplane"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1999-11", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "28", "bibliographicPageStart": "25", "bibliographicVolumeNumber": "43", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所特別資料"}, {"bibliographic_title": "Special Publicationa of National Aerospace Laboratory", "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": "航空宇宙技術研究所 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) 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": "National Aerospace Laboratory 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "NALでは無推進小型超音速実験機の空力形状を設計したところである。超音速での抵抗を減らすため、平面形アロー翼、ワープ翼、面積法則を適用した胴体、および自然層流(NLF)翼というデザインの考え方を採用した。NLF翼の設計のために、最適な圧力分布をサリーコードを用いて調べ、CFD(数値流体力学)逆問題設計法を独自に開発した。設計された翼は大きな層流領域を持つと推定した。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "NAL has just designed an aerodynamic configuration of the un-powered scaled supersonic experimental airplane. The following design concepts for reducing supersonic drag were incorporated: arrow planform, warp, area-ruled body and Natural Laminar Flow (NLF) wing. For the NLF wing design, an optimum design pressure distribution was investigated using SALLY code and a new inverse design method with CFD was originally developed. The designed wing was estimated to have large laminar region.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0001960008", "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: NAL SP-43", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory (NAL)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0289-260X", "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": "AN10097345", "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: 航空宇宙技術研究所"}]}, "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_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": "航空宇宙技術研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "航空宇宙技術研究所"}, {"subitem_text_value": "富士通"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}, {"subitem_text_language": "en", "subitem_text_value": "Fujitsu Ltd"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "吉田, 憲司"}], "nameIdentifiers": [{"nameIdentifier": "480608", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "真保, 雄一"}], "nameIdentifiers": [{"nameIdentifier": "480609", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "岩宮, 敏幸"}], "nameIdentifiers": [{"nameIdentifier": "480610", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "松島, 紀佐"}], "nameIdentifiers": [{"nameIdentifier": "480611", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yoshida, Kenji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480612", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shinbo, Yuichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480613", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwamiya, Toshiyuki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480614", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Matsushima, Kisa", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "480615", "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": "nalsp0043008.pdf", "filesize": [{"value": "779.6 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 779600.0, "url": {"label": "nalsp0043008.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/37405/files/nalsp0043008.pdf"}, "version_id": "d1357c45-dc90-4173-a2b9-b0122fb7ed53"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "境界層遷移", "subitem_subject_scheme": "Other"}, {"subitem_subject": "横流れ不安定", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD逆問題法", "subitem_subject_scheme": "Other"}, {"subitem_subject": "数値流体力学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ワープ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "自然層流翼設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "NLF 翼", "subitem_subject_scheme": "Other"}, {"subitem_subject": "層流領域", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空力形状", "subitem_subject_scheme": "Other"}, {"subitem_subject": "小型超音速実験機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "超音速抵抗", "subitem_subject_scheme": "Other"}, {"subitem_subject": "boundary layer transition", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "cross flow instability", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "CFD inverse method", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "computational fluid dynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "warp", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "natural laminar flow wing design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "NLF wing design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "laminar region", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamic configuration", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "scaled supersonic experimental airplane", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "supersonic drag", "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": "conference paper", "resourceuri": "http://purl.org/coar/resource_type/c_5794"}]}, "item_title": "航技研小型超音速実験機における自然層流翼設計", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "航技研小型超音速実験機における自然層流翼設計"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/37405", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "37405", "relation": {}, "relation_version_is_last": true, "title": ["航技研小型超音速実験機における自然層流翼設計"], "weko_shared_id": -1}
航技研小型超音速実験機における自然層流翼設計
https://jaxa.repo.nii.ac.jp/records/37405
https://jaxa.repo.nii.ac.jp/records/37405099fcdf5-8c64-4df7-8d7e-027c64edb51e
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0043008.pdf (779.6 kB)
|
|
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 | 航技研小型超音速実験機における自然層流翼設計 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層遷移 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 横流れ不安定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD逆問題法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ワープ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自然層流翼設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | NLF 翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 層流領域 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力形状 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型超音速実験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速抵抗 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer transition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cross flow instability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD inverse method | |||||
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 | warp | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | natural laminar flow wing design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | NLF wing design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laminar region | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scaled supersonic experimental airplane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic drag | |||||
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 | Natural laminar flow wing design of NAL's scaled supersonic experimental airplane | |||||
著者 |
吉田, 憲司
× 吉田, 憲司× 真保, 雄一× 岩宮, 敏幸× 松島, 紀佐× Yoshida, Kenji× Shinbo, Yuichi× Iwamiya, Toshiyuki× Matsushima, Kisa |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
富士通 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Fujitsu Ltd | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publicationa of National Aerospace Laboratory 巻 43, p. 25-28, 発行日 1999-11 |
|||||
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 | 航空宇宙技術研究所 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) 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 | National Aerospace Laboratory 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | NALでは無推進小型超音速実験機の空力形状を設計したところである。超音速での抵抗を減らすため、平面形アロー翼、ワープ翼、面積法則を適用した胴体、および自然層流(NLF)翼というデザインの考え方を採用した。NLF翼の設計のために、最適な圧力分布をサリーコードを用いて調べ、CFD(数値流体力学)逆問題設計法を独自に開発した。設計された翼は大きな層流領域を持つと推定した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | NAL has just designed an aerodynamic configuration of the un-powered scaled supersonic experimental airplane. The following design concepts for reducing supersonic drag were incorporated: arrow planform, warp, area-ruled body and Natural Laminar Flow (NLF) wing. For the NLF wing design, an optimum design pressure distribution was investigated using SALLY code and a new inverse design method with CFD was originally developed. The designed wing was estimated to have large laminar region. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001960008 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-43 |