高迎角時の方向操縦に関する一考察
1983 年 31 巻 350 号 p. 161-165
詳細
1983 年 31 巻 350 号 p. 161-165
Two Comments are given conceming yawing controls due to aileron at high angle of attack. Firstly, the lateral control departure parameter (LCDP) can be interpreted as a zero of the transfer function of aileron-to-yaw control. Secondly, the use of aileron is most effective for yaw control at extremely high angle of attack: numerical calculations are given for the recovery from flat-spin.
