Chapter 17: Problem 100
What is the effect of heat gain and heat loss on the entropy of the fluid during Rayleigh flow?
Chapter 17: Problem 100
What is the effect of heat gain and heat loss on the entropy of the fluid during Rayleigh flow?
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Get started for freeAir at 25 psia, \(320^{\circ} \mathrm{F}\), and Mach number \(\mathrm{Ma}=0.7\) flows through a duct. Calculate the velocity and the stagnation pressure, temperature, and density of air
Argon gas enters a constant cross-sectional area duct at \(\mathrm{Ma}_{1}=0.2, P_{1}=320 \mathrm{kPa},\) and \(T_{1}=400 \mathrm{K}\) at a rate of \(1.2 \mathrm{kg} / \mathrm{s} .\) Disregarding frictional losses, determine the highest rate of heat transfer to the argon without reducing the mass flow rate.
Nitrogen enters a steady-flow heat exchanger at \(150 \mathrm{kPa}, 10^{\circ} \mathrm{C},\) and \(100 \mathrm{m} / \mathrm{s},\) and it receives heat in the amount of \(120 \mathrm{kJ} / \mathrm{kg}\) as it flows through it. Nitrogen leaves the heat exchanger at 100 kPa with a velocity of \(200 \mathrm{m} / \mathrm{s}\) Determine the Mach number of the nitrogen at the inlet and the exit of the heat exchanger.
Compressed air from the compressor of a gas turbine enters the combustion chamber at \(T_{1}=700 \mathrm{K}, P_{1}\) \(=600 \mathrm{kPa},\) and \(\mathrm{Ma}_{1}=0.2\) at a rate of \(0.3 \mathrm{kg} / \mathrm{s} .\) Via combustion, heat is transferred to the air at a rate of \(150 \mathrm{kJ} / \mathrm{s}\) as it flows through the duct with negligible friction. Determine the Mach number at the duct exit, and the drop in stagnation pressure \(P_{01}-P_{02}\) during this process.
Combustion gases with \(k=1.33\) enter a converging nozzle at stagnation temperature and pressure of \(350^{\circ} \mathrm{C}\) and \(400 \mathrm{kPa},\) and are discharged into the atmospheric air at \(20^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\). The lowest pressure that will occur within the nozzle is \((a) 13 \mathrm{kPa}\) \((b) 100 \mathrm{kPa}\) \((c) 216 \mathrm{kPa}\) \((d) 290 \mathrm{kPa}\) \((e) 315 \mathrm{kPa}\)
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