WEKO3
アイテム
{"_buckets": {"deposit": "0bb0de95-ae68-43d9-81b5-83cdf73e929c"}, "_deposit": {"created_by": 1, "id": "36753", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "36753"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00036753", "sets": ["1891", "1915"]}, "author_link": ["477441", "477442", "477443", "477444"], "item_5_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "OREXの空力および空力加熱解析結果"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1996-01", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "26", "bibliographicPageStart": "17", "bibliographicVolumeNumber": "29", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所特別資料"}, {"bibliographic_title": "Special Publication 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 8 Jun. 1995 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 8 Jun. 1995 Tokyo Japan", "subitem_description_type": "Other"}]}, "item_5_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "HOPE(H-2ロケット打上型有翼回収機)開発に先立って3つの実験を行った。1994年2月4日にH-2のTF#1の機会にOREX(軌道再突入実験)を行い、再突入時の空気熱力学および空気力学の基礎データを取得しOREXの主目的のひとつの結果を報告した。空力熱力学については、飛行実験前に風洞実験値とFay\u0026Riddell法から導いた推定値との比較を評価した。実験後、以前に確認したFay\u0026Riddell法を使い飛行軌道から誘導した加熱率を推定した。そして熱解析モデルを使い澱み点の温度を計算し、飛行データの値と比較した。空気力学に関しては、推定値と飛行圧力データとを比較した。", "subitem_description_type": "Abstract"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Three experiments are performed preceding to the development of HOPE (H-2 Orbiting Plane). OREX (Orbital Reentry Experiment) was performed taking the opportunity of H-2 TF (Test Flight) No. 1 on Feb. 4, 1994. A result of one of the main purpose of OREX, acquisition of fundamental data of aerothermo- and aerodynamics during reentry is reported. As to aerothermodynamics, comparison between wind tunnel test data and values estimated from Fay \u0026 Riddell method was evaluated before a flight experiment. After the experiment, heating rate induced from flight orbit using Fay \u0026 Riddell method validated before was evaluated. And a temperature at the stagnation point was calculated using thermal-analysis model, then the value was compared with flight data. As to aerodynamics, flight pressure data was compared with estimated value.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0000110003", "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-29", "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": "宇宙開発事業団"}, {"subitem_text_value": "航空宇宙技術研究所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "National Space Development Agency of Japan"}, {"subitem_text_language": "en", "subitem_text_value": "National Aerospace Laboratory"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "下田, 孝幸"}], "nameIdentifiers": [{"nameIdentifier": "477441", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "松崎, 貴至"}], "nameIdentifiers": [{"nameIdentifier": "477442", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Shimoda, Takayuki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "477443", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Matsuzaki, Takashi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "477444", "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": "nalsp0029003.pdf", "filesize": [{"value": "769.3 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 769300.0, "url": {"label": "nalsp0029003.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/36753/files/nalsp0029003.pdf"}, "version_id": "605959ef-e704-4700-9030-27050e69b130"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "OREX", "subitem_subject_scheme": "Other"}, {"subitem_subject": "軌道再突入実験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空気熱力学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "空気力学", "subitem_subject_scheme": "Other"}, {"subitem_subject": "HOPE", "subitem_subject_scheme": "Other"}, {"subitem_subject": "H-2ロケット打上型有翼回収機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "風洞", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱解析モデル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "澱み点", "subitem_subject_scheme": "Other"}, {"subitem_subject": "飛行圧力データ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "高エンタルピー流れ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "OREX", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "orbital reentry experiments", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerothermodynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "aerodynamics", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "HOPE", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "H 2 orbiting plane", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "wind tunnel", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "thermal analysis model", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "stagnation point", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flight pressure data", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "high enthalpy flow", "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": "The result of an analysis of aerothermo and aerodynamics of OREX", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "The result of an analysis of aerothermo and aerodynamics of OREX", "subitem_title_language": "en"}]}, "item_type_id": "5", "owner": "1", "path": ["1891", "1915"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/36753", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "36753", "relation": {}, "relation_version_is_last": true, "title": ["The result of an analysis of aerothermo and aerodynamics of OREX"], "weko_shared_id": -1}
The result of an analysis of aerothermo and aerodynamics of OREX
https://jaxa.repo.nii.ac.jp/records/36753
https://jaxa.repo.nii.ac.jp/records/367534eb3b975-a7e3-4e80-9cb0-c4ffe3446b61
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0029003.pdf (769.3 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 | The result of an analysis of aerothermo and aerodynamics of OREX | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道再突入実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気熱力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2ロケット打上型有翼回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱解析モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 澱み点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行圧力データ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高エンタルピー流れ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital reentry experiments | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerothermodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 orbiting plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal analysis model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stagnation point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight pressure data | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy flow | |||||
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 | ||||||
その他のタイトル | OREXの空力および空力加熱解析結果 | |||||
著者 |
下田, 孝幸
× 下田, 孝幸× 松崎, 貴至× Shimoda, Takayuki× Matsuzaki, Takashi |
|||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 Publication of National Aerospace Laboratory 巻 29, p. 17-26, 発行日 1996-01 |
|||||
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 8 Jun. 1995 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 8 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | HOPE(H-2ロケット打上型有翼回収機)開発に先立って3つの実験を行った。1994年2月4日にH-2のTF#1の機会にOREX(軌道再突入実験)を行い、再突入時の空気熱力学および空気力学の基礎データを取得しOREXの主目的のひとつの結果を報告した。空力熱力学については、飛行実験前に風洞実験値とFay&Riddell法から導いた推定値との比較を評価した。実験後、以前に確認したFay&Riddell法を使い飛行軌道から誘導した加熱率を推定した。そして熱解析モデルを使い澱み点の温度を計算し、飛行データの値と比較した。空気力学に関しては、推定値と飛行圧力データとを比較した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Three experiments are performed preceding to the development of HOPE (H-2 Orbiting Plane). OREX (Orbital Reentry Experiment) was performed taking the opportunity of H-2 TF (Test Flight) No. 1 on Feb. 4, 1994. A result of one of the main purpose of OREX, acquisition of fundamental data of aerothermo- and aerodynamics during reentry is reported. As to aerothermodynamics, comparison between wind tunnel test data and values estimated from Fay & Riddell method was evaluated before a flight experiment. After the experiment, heating rate induced from flight orbit using Fay & Riddell method validated before was evaluated. And a temperature at the stagnation point was calculated using thermal-analysis model, then the value was compared with flight data. As to aerodynamics, flight pressure data was compared with estimated value. | |||||
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: AA0000110003 | |||||
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-29 |