Chapter 17: Problem 16
Is it realistic to approximate that the propagation of sound waves is an isentropic process? Explain.
Chapter 17: Problem 16
Is it realistic to approximate that the propagation of sound waves is an isentropic process? Explain.
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Get started for freeAir enters an approximately frictionless duct with \(V_{1}=70 \mathrm{m} / \mathrm{s}, T_{1}=600 \mathrm{K},\) and \(P_{1}=350\) kPa. Letting the exit temperature \(T_{2}\) vary from 600 to 5000 \(\mathrm{K},\) evaluate the entropy change at intervals of \(200 \mathrm{K},\) and plot the Rayleigh line on a \(T\) -s diagram.
Air flows with negligible friction through a \(4-\) in-diameter duct at a rate of 5 lbm/s. The temperature and pressure at the inlet are \(T_{1}=800 \mathrm{R}\) and \(P_{1}=30\) psia, and the Mach number at the exit is \(\mathrm{Ma}_{2}=1 .\) Determine the rate of heat transfer and the pressure drop for this section of the duct
Air enters a nozzle at 30 psia, \(630 \mathrm{R}\), and a velocity of \(450 \mathrm{ft} / \mathrm{s}\). Approximating the flow as isentropic, determine the pressure and temperature of air at a location where the air velocity equals the speed of sound. What is the ratio of the area at this location to the entrance area?
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What would happen if we tried to further accelerate a supersonic fluid with a diverging diffuser?
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