並列タイトル等USB-パワード・リフトSTOL機縦空力係数非線形モデル
タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-995
一般注記A longitudinal nonlinear aerodynamic model form for USB-STOL aircraft has been prepared. Static part and the dynamic part of the model form were drawn separately. The static part model form was then verified by fitting it to wing tunnel test data of the NAL-STOL experimental airplane “ASUKA”. For the dynamic part, three types of model form are proposed as candidates. They differ from each other in the method of modeling the lag of downwash: In the first model the lag is simulated precisely, in the second model it is approximated from the first lag, and in the third model, the lag is neglected. A comparison of the results of dynamic flight simulation with these three models comes to the conclusion that the second model is the most appropriate for parameter identification from flight test data.
資料番号: NALTR0995000
レポート番号: NAL TR-995
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45254&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ