Drag, D = 1/2*Drag coefficient*density of air*velocity^2*Frontal area
Where,
Density of air ≈ 1.225 kg/m^3
Velocity = 55 mph = 24.5872 m/s
Drag coefficient = 0.21
Frontal area = 30 ft^2 = 2.78709 m^2
Substituting;
D = 0.5*0.21*1.225*24.5872^2*2.78709 = 216.72 N