A light plane flies at 720 km/hr in standard air at an altitude of 1000 m. Determine the stagnation pressure at the leading edge of the wing. Take, $$P_{air} = 9.0 \times 10^4 N/m^2$$, $$\rho = 1.1 kg/m^3$$

A

90 kPa

B

119 kPa

C

112 kPa

D

100 kPa