Research Article
Effect of the Simultaneous Variation in Blade Root Chord Length and Blade Taper on Helicopter Flight Control Effort
Figure 6
Effect of simultaneous variation in blade root chord and blade taper on the control effort (i.e., control energy) of the FCS of a helicopter.
(a) Original plot for hover |
(b) Zoomed plot for hover |
(c) Original plot for 40-knot SLFC |
(d) Zoomed plot for 40-knot SLFC |
(e) Original plot for 80-knot SLFC |
(f) Zoomed plot for 80-knot SLFC (SLFC: straight-and-level flight condition) |