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A perfect gas flows through a nozzle when it expends in a reversible adiabatic manner, the inlet conditions are 22 bar,, 500oc, 38 m/s. At exit the pressure is 2 bar. Evaluate the exit velocity and exit area if the flow rate is 4 Kg/s. Take R = 190J/KgK and γ = 1.35
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Air at 1 atm, 300K, and Re = 50,000: a. Flow across the cylinder with a diameter of 10 cm. b. Flow inside a tube with a diameter of 10 cm. c. flow along the flat plate of
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