U1 U2 A3 Ue T. Ac 1 2 3 15 A+ the enter of a con veging-diverging no2zle; To= Sol k and Po=300 fa. C iS throat section nd throat Conditions cre valid here. There 3 a nomual shock from the throat section to the 1s+ section. The cross Section 2 s the flow region after shock. A1-4m, A2=2m2 and A3=3m. Calculate the physical values (pressre density, Speed Sound e loerty iMach number, Stagnation Pressure,s tagnation temp. and stagration dansity) at section C,12 and 3. Create table and indicate the physical values. Between 2-3, flow is isentropic. Between 1-2, you can use shock equations