Effect of the Simultaneous Variation in Blade Root Chord Length and Blade Taper on Helicopter Flight Control Effort

<div>Effect of simultaneous variations in blade root chord and blade taper on some states for 40-knot SLFC.</div>

International Journal of Aerospace Engineering

Figure 7: Effect of the Simultaneous Variation in Blade Root Chord Length and Blade Taper on Helicopter Flight Control Effort 