Question
In a supersonic nozzle flow, the exit-to-throat area ratio is 10, p 0 = 10 atm. and the backpressure P B = 0.04 atm. Calculate
In a supersonic nozzle flow, the exit-to-throat area ratio is 10, p 0 = 10 atm. and the backpressure P B = 0.04 atm. Calculate the angle 8 through which the low is deflected immediately after leaving the edge (or lip) of the nozzle exit.
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Thermodynamics An Interactive Approach
Authors: Subrata Bhattacharjee
1st edition
130351172, 978-0130351173
