Consider a convergent-divergent nozzle with an exit-to-throat area ratio of 1.53 . The reservoir pressure is 1 atm. Assuming isentropic flow, except for the possibility of a normal shock wave inside the nozzle, calculate the exit Mach number when the exit pressure pe is (a) 0.94  atm (b) 0.886  atm (c) 0.75  atm (d) 0.154  atm | Numerade
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SOLVED: A nozzle is designed to expand air from a chamber in which the pressure and temperature are 800 kPa and 40^∘ C respectively to a Mach number of 2.5 . The throat area of this nozzle is to be 0.1  m^2. Find: 1. The exit area of the nozzle 2. The mass flow rate through the nozzle when operating at design conditions 3. The back pressure at which there will be a normal shock wave on the exit plane of the nozzle 4. The range of back pressures over which expansion waves will occur outside the n
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