@techreport{oai:jaxa.repo.nii.ac.jp:00039764,
 author = {穂積, 弘毅 and 坂井, 紀穂 and Hozumi, Koki and Sakai, Toshiho},
 month = {Apr},
 note = {航空宇宙技術研究所の実験用航空機であるドルニエ社製Do228型機の飛行試験データからV-γ線図を作成し、同図を用いて飛行性能値のみでなく縦の運動を支配する主要なパラメータ(縦の微係数)を推定した。また、同機の風洞試験データをもとにした数学モデルより算出したパラメータと飛行試験から得られたV-γ線図により算出されたパラメータとを比較し、数学モデルの検証を行った。さらに、縦の微係数に含まれる誤差の影響を論じた。, In this study, the flying qualities of the flight research airplane Do228 were evaluated. By performing some flight tests using a Do228, the V-gamma diagrams with some configurations were drawn out. The flight performance was obtained, and some longitudinal aerodynamic derivatives such as X(sub )u, X(sub w), Z(sub u) and Z(sub w) were estimated from the performance. The parameter errors were examined by comparing the above parameters with those based on the wind tunnel tests. According to the results, the accuracy of the parameters estimated from V-gamma diagrams was sufficient to discuss the longitudinal dynamics., 資料番号: AA0000447000, レポート番号: NAL TR-1288},
 title = {V-γ線図による実験用航空機Do228の飛行性評価},
 year = {1996}
}