In the Figure below, the density of fluid 1, p1-700 kg/m and the density of fluid 2, p2=950 kg/m In addition, h=0.9 m and h2=0.75 m. Assume g=9.81 m/s and Patm =101.3 kPa. By first writing the manometer equation for computing the pressure at point A at the bottom of the container, the absolute pressure at Point A in kPa is Fluid 1 atm P Fluid 2 P A An aircraft is flying at an altitude of 9000 m above a city. If the ground atmospheric pressure in the city is 101.2 kPa, what will be the pressure at the altitude where the aircraft is flying in kPa. Assume g=9.81 m/s and that the average density of the air is 1.05 kg/m.