If the ailerons are deflected to 10°, compared to 5°, this will cause:
a. An increased angle of bank
b. An increased rate of roll
c. No change to either bank angle or roll rate
d. A reduction in the adverse yawing moment
a. An increased angle of bank
b. An increased rate of roll
c. No change to either bank angle or roll rate
d. A reduction in the adverse yawing moment