I would use miles
Because miles will give you less of an answer
Answer:
C. Angle of Attack.
Explanation:
The pilot must adjust the angle of attack parameter. The angle of attack of this plane to get to the desired lift coefficient.
And thus, we have
Lift = Weight
V=IR
Potential Difference (v)= Current (A) * Resistance (Ω)
As V increases, R also increases.
