{"created":"2023-06-20T15:11:29.376948+00:00","id":41158,"links":{},"metadata":{"_buckets":{"deposit":"fd0dce64-62d6-4f87-be1c-c46d930d427d"},"_deposit":{"created_by":1,"id":"41158","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41158"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041158","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["450831","450830"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Identifying the NAL Spaceplane aerodynamic model using dynamic wind tunnel tests"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"41","bibliographicPageStart":"1","bibliographicVolumeNumber":"1171","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":"従来より航空宇宙技術研究所(NAL)において研究が行われている動的飛行試験による航空機空力特性同定法をケーブル支持方式動的風洞試験に適用し、NALスペースプレーンの空力モデル同定を行った。同定されたモデルの静的パラメータについては動的試験に先だって行われた静的風洞試験により推定された結果との、動的パラメータについては理論推定された結果との比較を行った。また、静的および動的パラメータの総合評価のため、同定したモデルに基づき非線形計算機シミュレーションを行い、動的風洞試験記録データと比較した。その結果良好な同定が行われ、動的風洞試験による空力モデル同定の有効性が示された。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An aerodynamic model identification technique utilized by the National Aerospace Laboratory (NAL) was applied to dynamic wind tunnel tests using a cable mounted model to extract aerodynamic parameters of the NAL Spaceplane. The estimated static parameters were evaluated by comparisons with static wind tunnel test results, whereas those for the dynamic parameters with theoretically estimated values. In addition, mathematical flight simulations using both static and dynamic parameters were conducted for the total evaluation. The simulated results were subsequently compared with the wind tunnel test data, and satisfactory correlation was achieved; thereby demonstrating the effectiveness of the dynamic tests.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004188000","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-1171","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"動的風洞試験グループ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Dynamic Wind Tunnel Test Group","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":"naltr01171.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01171.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41158/files/naltr01171.pdf"},"version_id":"75c5aad0-7484-4920-aae2-2fc95ea91879"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力モデル同定","subitem_subject_scheme":"Other"},{"subitem_subject":"空力パラメータ同定","subitem_subject_scheme":"Other"},{"subitem_subject":"空力微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"動的微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"安定微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"運動解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行状態シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性計測","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーブルマウント模型","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞模型支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"動的模型支持","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"NALスペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic model identification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic parameter identification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight dynamics simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cable mounted model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic model support","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NAL space 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":"ケーブル支持動的風洞試験によるNALスペースプレーンの空力モデル同定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ケーブル支持動的風洞試験によるNALスペースプレーンの空力モデル同定"}]},"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":"41158","relation_version_is_last":true,"title":["ケーブル支持動的風洞試験によるNALスペースプレーンの空力モデル同定"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:58.282824+00:00"}