1.

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, Pair = 9.0 × 104 N/m2, ρ = 1.1 kg/m3.

A. 90 kPa
B. 119 kPa
C. 112 kPa
D. 100 kPa
Answer» D. 100 kPa


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