A passenger jet aircraft is flying 90 mph at 10,000 ft altitude. At a minimum pressure point on a surface of the wing, the airspeed 100 mph is measured. (a) Calculate the pressure, both in "psig" and "psia," at this minimum pressure point on a surface of the wing. (b) Calculate the pressure, both in "psig" and "psia," at the leading edge of the wing, where the airspeed measured is zero (stagnation point). Hints ... Apply Bernoulli's equation between free stream, stagnation point, and minimum pressure point.