{"created":"2023-06-20T15:10:39.957813+00:00","id":40243,"links":{},"metadata":{"_buckets":{"deposit":"8bacc218-9a7e-478d-b73b-aec62d56a0c0"},"_deposit":{"created_by":1,"id":"40243","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40243"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040243","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["446995","446996","446994","446997","446992","446993"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル(英)","attribute_value_mlt":[{"subitem_alternative_title":"Estimating aerodynamic characteristics of the ALFLEX vehicle using flight test data and comparison with wind tunnel test data"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"29","bibliographicPageStart":"1","bibliographicVolumeNumber":"1353","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"小型自動着陸実験(ALFLEX)の目的の1つにデルタ翼チップフィン形態機の低速空力特性推定があり、そのためのα、βスイープ試験、舵面加振試験などの空力特性推定試験が懸吊飛行および自動着陸飛行中に実施された。豪州ウーメラ実験場において取得されたこれらのデータを解析することにより実験機の空力特性を推定し、実験に先立って行われたいくつかの風洞試験の結果と比較した。その結果、飛行試験による推定特性と、実験機の制御系設計に使用された基準風洞試験結果との差は概ね変動誤差の範囲内であったが、一部の風洞試験結果との間には大きな差が見られた。この差は風洞試験における模型支持方法、模型剛性、模型形状(胴上開口部の有無、脚形状)などの影響の補正が充分でないことによると考えられる。また、懸吊飛行試験はアンビリカルケーブルが原因と考えられるジンバル角の計測誤差の影響により、一部の推定結果にばらつきが見られたが、これを改善することにより空力特性推定のための有効な手法となり得ることが確認された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"One of the purposes of the Automatic Landing Flight Experiment (ALFLEX) is to estimate the aerodynamic characteristics of a vehicle with a delta wing and tip fins. The tests for this purpose, such as alpha and beta sweep tests and control surface excitation test, were conducted during the hanging flights and automatic landing flights. By analyzing the flight test data obtained at the Woomera test site in Australia, the aerodynamic characteristics of the ALFLEX vehicle were estimated and the results were compared with ones predicted by several wind tunnel tests. As a result, the differences between the estimated characteristics and the results of the basic wind tunnel test were within the variation. Some other wind tunnel tests, however, showed significantly different results from the flight tests. These differences seemed to be caused by errors of the wind tunnel tests due to, for example, the effect of the supporting device. Although the results of the hanging flights were scattered due to measurement errors caused by the effects of an umbilical cable, the method will be useful if the problem can be solved such as by using an inner battery.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001573000","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-1353","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_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 制御部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"宇宙開発事業団"}]},"item_3_text_7":{"attribute_name":"著者所属(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Control Systems Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"柳原, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"重見, 仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"水藤, 貴靖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagihara, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shigemi, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suito, Takanobu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001353.pdf","filesize":[{"value":"3.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001353.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40243/files/naltr0001353.pdf"},"version_id":"431aff85-a9ad-4e87-b416-b9bf6de03b11"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ALFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"小型自動着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験データ","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"デルタ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"チップフィン","subitem_subject_scheme":"Other"},{"subitem_subject":"懸吊飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"ALFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Automatic Landing Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic property","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"tip fin","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hanging flight test","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"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"飛行試験データによるALFLEX実験機の空力特性推定と風洞試験データとの比較評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"飛行試験データによるALFLEX実験機の空力特性推定と風洞試験データとの比較評価"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40243","relation_version_is_last":true,"title":["飛行試験データによるALFLEX実験機の空力特性推定と風洞試験データとの比較評価"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:16:27.845504+00:00"}