Chapter 17: Problem 70
Are the isentropic relations of ideal gases applicable for flows across \((a)\) normal shock waves, \((b)\) oblique shock waves, and ( \(c\) ) Prandtl-Meyer expansion waves?
Chapter 17: Problem 70
Are the isentropic relations of ideal gases applicable for flows across \((a)\) normal shock waves, \((b)\) oblique shock waves, and ( \(c\) ) Prandtl-Meyer expansion waves?
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Get started for freeFor an oblique shock to occur, does the upstream flow have to be supersonic? Does the flow downstream of an oblique shock have to be subsonic?
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 \(150 \mathrm{kJ} / \mathrm{kg}\) as it flows through it. The nitrogen leaves the heat exchanger at \(100 \mathrm{kPa}\) with a velocity of \(200 \mathrm{m} / \mathrm{s}\) Determine the stagnation pressure and temperature of the nitrogen at the inlet and exit states.
Consider subsonic Rayleigh flow that is accelerated to sonic velocity \((\mathrm{Ma}=1)\) at the duct exit by heating. If the fluid continues to be heated, will the flow at duct exit be supersonic, subsonic, or remain sonic?
Assuming you have a thermometer and a device to measure the speed of sound in a gas, explain how you can determine the mole fraction of helium in a mixture of helium gas and air.
Air 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
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