5.2 5.3 Consider a downward ramp (convex corner) with angle = 10 as shown in the Figure below. The incoming airflow is supersonic with M = 1.5, p = 105 Pa, T = 298 K. Assume air behaves like an ideal gas with y=1.4 and R=287J/kg-K. M, P1, P1, T1 M2, P2, P2, T2 1) Determine the conditions past the expansion fan. Use the Prandtl-Meyer function to compute v(M) exactly, but its zoomed-in plot below to get M from (M). 25 24 23 22 21 20 19 16 17 16 15 20 Provide the Mach number with three digits of precision (of the form X.YZEP): M = Provide the pressure (in Pascals) with three digits of precision (of the form X.YZEP): p2= Provide the temperature with three digits of precision (of the form X.YZeP): T = Provide the density with two digits of precision (of the form X.YeP): P = 2) What is the total pressure loss 1-po/Po,? Provide your answer with two digits of precision (of the form X.YeP). v(M) [deg]