Chapter 9: Problem 141
Calculate the exergy destruction for each process of Stirling cycle of Prob. \(9-74,\) in \(\mathrm{kJ} / \mathrm{kg}\)
Chapter 9: Problem 141
Calculate the exergy destruction for each process of Stirling cycle of Prob. \(9-74,\) in \(\mathrm{kJ} / \mathrm{kg}\)
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Get started for freeAn aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of \(10 .\) Heat is added to the cycle at a rate of \(500 \mathrm{kW} ;\) air passes through the engine at a rate of \(1 \mathrm{kg} / \mathrm{s} ;\) and the air at the beginning of the compression is at \(70 \mathrm{kPa}\) and \(0^{\circ} \mathrm{C}\). Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature.
An ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is \(95 \mathrm{kPa}\) and \(20^{\circ} \mathrm{C}\). If the maximum temperature in the cycle is not to exceed \(2200 \mathrm{K}\) determine \((a)\) the thermal efficiency and \((b)\) the mean effective pressure. Assume constant specific heats for air at room temperature.
How does a diesel engine differ from a gasoline engine?
A four-cylinder two-stroke 2.4 -L diesel engine that operates on an ideal Diesel cycle has a compression ratio of 22 and a cutoff ratio of \(1.8 .\) Air is at \(70^{\circ} \mathrm{C}\) and \(97 \mathrm{kPa}\) at the beginning of the compression process. Using the cold-airstandard assumptions, determine how much power the engine will deliver at \(3500 \mathrm{rpm}\)
What cycle is composed of two isothermal and two constant-volume processes?
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