@techreport{oai:jaxa.repo.nii.ac.jp:00043789,
 author = {河崎, 俊夫 and 河本, 巌 and KAWASAKI, Toshio and KAWAMOTO, Iwao},
 month = {Jul},
 note = {The present paper deals with the method of estimation of aerodynamic stability derivatives, especially dynamic stability derivatives, for the free flight model FFM-10, and presents these estimated results.  The method we employed is mostly based on the so-called apparent mass method. However, according to the original method (ref. 5), the aerodynamic force acting on each component of a vehicle is estimated by the slender body theory ; as a result, stability derivatives of the whole vehicle composed of these component values are thought to have the same accuracy as slender body theory, and are independent of the Mach number. In order to avoid this defect, we employed a supersonic linearized theory in calcuating the aerodynamic force acting on wing component whose contribution to the derivatives for FFM-1O is most important.  Moreover, improvement of precision for these derivatives is attempted by taking the result of static wind tunnel tests into account., 資料番号: NALTM0205000, レポート番号: NAL TM-205},
 title = {自動飛行模型FFM-10の動安定微係数の推定について},
 year = {1971}
}