Air is drawn into a small open-circuit wind tunnel as shown in Fig. 3. Atmospheric pressure is 120.2 kPa (abs) and the temperature is 27°C. If viscous effects are negligible, determine: (a) The pressure at the stagnation point on the nose of the airplane. (b) The manometer reading, h, for the manometer attached to the static pressure tap within the test section of the wind tunnel if the air velocity within the test section is 75 m/s. Test Inlet nozzle section -Diffuser- Fan 73) Inlet Water

Fast pls solve this question correctly in 5 min pls I will give u like for sure Sub A vertical plate is submerged in water and has the indicated shape. Express how to approximate the hydrostatic force against one side of the plate by an integra and evaluate it. Use a Riemann sum.

Find the fluid force on an equilateral triangle facing down with a width of 2 feet

(Just Question a.) A water filled pipe has water flowing at v1= 5.90 m/s in a section of pipe where the diameter is d1= 20.2 cm and the pressure is known to be P1= 7.00×104 N/m2 above atmospheric pressure.     If the pipe carries the water 3.5 meters up hill without any change in diameter, what is the new absolute pressure within the pipe? After flowing up the hill described above, the pipe narrows to 80% of its original radius, what will be the new water velocity (v2) in the pipe? What will be the absolute pressure (P3) in the smaller pipe?   a. What is the volume flow rate through the smaller pipe?