Please compute the solution of the given Problem
Problem- An airplane flies at an elevation of 5000 ft in standard atmosphere. The pressure difference indicated by the Pitot-static probe attached to the fuselage is 0.1213 psi.
Part 1- What is the velocity of the airplane? (The density of air at this altitude is 0.046 lbm/ft3)
I need expert's assistance to compute the velocity of the airplane.