准一维流动.Consider a convergent-divergent duct with exit and thr
准一维流动.
Consider a convergent-divergent duct with exit and throat areas of 0.5 m2 and 0.25m2,respectively.The inlet reservoir pressure is 1 atm and the exit static pressure is 0.6 atm.For this pressure ratio,the flow will be supersonic in a portion of the nozzle,terminating with a normal shock inside the nozzle.Calculate the local area ratio (A/A*) at which the shock is located inside the nozzle.