WEKO3
アイテム
{"_buckets": {"deposit": "6a6e159a-cffd-4d68-a928-a9c5094c70aa"}, "_deposit": {"created_by": 1, "id": "44931", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "44931"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00044931", "sets": ["1893", "1917"]}, "author_link": ["472017", "472022", "472021", "472018", "472020", "472019"], "item_3_alternative_title_1": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "回転式速度ベクトル測定装置"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1981-06", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "19", "bibliographicVolumeNumber": "674", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所報告"}, {"bibliographic_title": "Technical Report of National Aerospace Laboratory TR-674", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In the NAL 6m low speed wind tunnel flow field measurements have been carried out by traversing only one yawmeter probe. But it consumes too much time to measure the flow field around a full-scale aircraft model with one probe, so a velocity vector measuring system with 13 asymmetric-wedge type yawmeters was developed in order to survey the flow field around the empennage of the NAL STOL research aircract model. The rotational angle of the 13 probes and the setting angle of this system are automatically controlled following the sequence previously programmed into a mini-computer system. As the principle of measurement used in this system is almost the same as that reported in NAL TR-594, this paper mainly describes the hardware of this system, the control modes, the data reduction, and the data processing. The accuracy of the flow angle measurement turned out to be satisfactory, but measurements of dynamic pressure and static pressure were less accurate. This paper concludes with an example of measurements taken of the flow field around the empennage of the NAL STOL research aircraft model.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTR0674000", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: NAL TR-674", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory(NAL)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0389-4010", "subitem_source_identifier_type": "ISSN"}]}, "item_3_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: NAL-MATCH"}]}, "item_3_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_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_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: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第二部"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}, {"subitem_text_language": "en", "subitem_text_value": "Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "中谷, 輝臣"}], "nameIdentifiers": [{"nameIdentifier": "472017", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "星野, 秀雄"}], "nameIdentifiers": [{"nameIdentifier": "472018", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "野口, 正芳"}], "nameIdentifiers": [{"nameIdentifier": "472019", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NAKAYA, Teruomi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "472020", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "HOSHINO, Hideo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "472021", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NOGUCHI, Masayoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "472022", "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": "2020-01-29"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltr00674.pdf", "filesize": [{"value": "1.7 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1700000.0, "url": {"label": "naltr00674.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/44931/files/naltr00674.pdf"}, "version_id": "acc8a983-bde0-4f41-8d96-e359fae066d6"}]}, "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": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "A Velocity Vector Measuring System with 13 Asymmetric-Wedge Type Yewmeters", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "A Velocity Vector Measuring System with 13 Asymmetric-Wedge Type Yewmeters", "subitem_title_language": "en"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1917"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/44931", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "44931", "relation": {}, "relation_version_is_last": true, "title": ["A Velocity Vector Measuring System with 13 Asymmetric-Wedge Type Yewmeters"], "weko_shared_id": -1}
A Velocity Vector Measuring System with 13 Asymmetric-Wedge Type Yewmeters
https://jaxa.repo.nii.ac.jp/records/44931
https://jaxa.repo.nii.ac.jp/records/44931eebd0598-6b22-4f2b-8da1-782117d272bb
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr00674.pdf (1.7 MB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A Velocity Vector Measuring System with 13 Asymmetric-Wedge Type Yewmeters | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 回転式速度ベクトル測定装置 | |||||
著者 |
中谷, 輝臣
× 中谷, 輝臣× 星野, 秀雄× 野口, 正芳× NAKAYA, Teruomi× HOSHINO, Hideo× NOGUCHI, Masayoshi |
|||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-674 巻 674, p. 19, 発行日 1981-06 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the NAL 6m low speed wind tunnel flow field measurements have been carried out by traversing only one yawmeter probe. But it consumes too much time to measure the flow field around a full-scale aircraft model with one probe, so a velocity vector measuring system with 13 asymmetric-wedge type yawmeters was developed in order to survey the flow field around the empennage of the NAL STOL research aircract model. The rotational angle of the 13 probes and the setting angle of this system are automatically controlled following the sequence previously programmed into a mini-computer system. As the principle of measurement used in this system is almost the same as that reported in NAL TR-594, this paper mainly describes the hardware of this system, the control modes, the data reduction, and the data processing. The accuracy of the flow angle measurement turned out to be satisfactory, but measurements of dynamic pressure and static pressure were less accurate. This paper concludes with an example of measurements taken of the flow field around the empennage of the NAL STOL research aircraft model. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0674000 | |||||
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 TR-674 |