Chapter 8: Problem 7
What is the second-law efficiency? How does it differ from the first-law efficiency?
Chapter 8: Problem 7
What is the second-law efficiency? How does it differ from the first-law efficiency?
All the tools & learning materials you need for study success - in one app.
Get started for freeArgon gas enters an adiabatic compressor at \(120 \mathrm{kPa}\) and \(30^{\circ} \mathrm{C}\) with a velocity of \(20 \mathrm{m} / \mathrm{s}\) and exits at \(1.2 \mathrm{MPa}\) \(530^{\circ} \mathrm{C},\) and \(80 \mathrm{m} / \mathrm{s}\). The inlet area of the compressor is \(130 \mathrm{cm}^{2} .\) Assuming the surroundings to be at \(25^{\circ} \mathrm{C}\), determine the reversible power input and exergy destroyed.
An insulated vertical piston-cylinder device initially contains \(15 \mathrm{kg}\) of water, \(13 \mathrm{kg}\) of which is in the vapor phase. The mass of the piston is such that it maintains a constant pressure of \(300 \mathrm{kPa}\) inside the cylinder. Now steam at \(2 \mathrm{MPa}\) and \(400^{\circ} \mathrm{C}\) is allowed to enter the cylinder from a supply line until all the liquid in the cylinder is vaporized. Assuming the surroundings to be at \(25^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\), determine \((a)\) the amount of steam that has entered and ( \(b\) ) the exergy destroyed during this process.
Obtain the following information about a power plant that is closest to your town: the net power output; the type and amount of fuel used; the power consumed by the pumps, fans, and other auxiliary equipment; stack gas losses; temperatures at several locations; and the rate of heat rejection at the condenser. Using these and other relevant data, determine the rate of irreversibility in that power plant.
Writing the first- and second-law relations and \(\operatorname{sim}-\) plifying, obtain the reversible work relation for a uniformflow system that exchanges heat with the surrounding medium at \(T_{0}\) in the amount of \(Q_{0}\) as well as a heat reservoir at \(T_{R}\) in the amount of \(Q_{R^{*}}\) (Hint: Eliminate \(Q_{0}\) between the two equations.)
Combustion gases enter a gas turbine at \(627^{\circ} \mathrm{C}\) and \(1.2 \mathrm{MPa}\) at a rate of \(2.5 \mathrm{kg} / \mathrm{s}\) and leave at \(527^{\circ} \mathrm{C}\) and \(500 \mathrm{kPa} .\) It is estimated that heat is lost from the turbine at a rate of \(20 \mathrm{kW}\). Using air properties for the combustion gases and assuming the surroundings to be at \(25^{\circ} \mathrm{C}\) and 100 kPa, determine \((a)\) the actual and reversible power outputs of the turbine, (b) the exergy destroyed within the turbine, and \((c)\) the second-law efficiency of the turbine.
What do you think about this solution?
We value your feedback to improve our textbook solutions.