Chapter 17: Problem 7
Determine the stagnation temperature and stagnation pressure of air that is flowing at \(36 \mathrm{kPa}, 238 \mathrm{K},\) and \(325 \mathrm{m} / \mathrm{s}\).
Chapter 17: Problem 7
Determine the stagnation temperature and stagnation pressure of air that is flowing at \(36 \mathrm{kPa}, 238 \mathrm{K},\) and \(325 \mathrm{m} / \mathrm{s}\).
All the tools & learning materials you need for study success - in one app.
Get started for freeAir enters a rectangular duct at \(T_{1}=300 \mathrm{K}, P_{1}=\) \(420 \mathrm{kPa},\) and \(\mathrm{Ma}_{1}=2 .\) Heat is transferred to the air in the amount of \(55 \mathrm{kJ} / \mathrm{kg}\) as it flows through the duct. Disregarding frictional losses, determine the temperature and Mach number at the duct exit.
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
Steam flows through a device with a pressure of 120 psia, a temperature of \(700^{\circ} \mathrm{F}\), and a velocity of \(900 \mathrm{ft} / \mathrm{s}\). Determine the Mach number of the steam at this state by assuming ideal-gas behavior with \(k=1.3\).
Plot the mass flow parameter \(\dot{m} \sqrt{R T_{0}} /\left(A P_{0}\right)\) versus the Mach number for \(k=1.2,1.4,\) and 1.6 in the range of \(0 \leq \mathrm{Ma} \leq 1\)
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.
What do you think about this solution?
We value your feedback to improve our textbook solutions.