The tail liftcurveslope as determined from the panel model may require adjustment in order to apply the test results.
为了应用试验结果，根据翼段模型试验确定的平尾升力曲线斜率可能要作些修正。
2
The results show that the flying qualities are most sensitive to variations of the longitudinal control effectiveness and the moment of inertia besides a little to variation of the liftcurveslope.
Thus, in the worst case of zero leading-edge suction, the drag-due-to-lift factor K is simply the inverse of the slope of the life curve (in radians), as previously determined.