Chapter 9: Problem 5
Define the compression ratio for reciprocating engines.
Chapter 9: Problem 5
Define the compression ratio for reciprocating engines.
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Get started for freeAn air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed piston-cylinder system and is composed of the following five processes: \(1-2 \quad\) Isentropic compression with a compression ratio \(r=V_{1} / V_{2}\) \(2-3 \quad\) Constant volume heat addition with a pressure ratio, \\[ r_{p}=P_{3} / P_{2} \\] \(3-4 \quad\) Constant pressure heat addition with a volume ratio \\[ r_{c}=V_{4} / V_{3} \\] \(4-5 \quad\) Isentropic expansion while work is done until \(V_{5}=V_{1}\) \(5-1 \quad\) Constant volume heat rejection to the initial state (a) Sketch the \(P\) -V and \(T\) -s diagrams for this cycle. (b) Obtain an expression for the cycle thermal efficiency as a function of \(k, r, r_{c},\) and \(r_{p}\) (c) Evaluate the limit of the efficiency as \(r_{p}\) approaches unity and compare your answer with the expression for the Diesel cycle efficiency. (d) Evaluate the limit of the efficiency as \(r_{c}\) approaches unity and compare your answer with the expression for the Otto cycle efficiency.
An ideal Otto cycle with air as the working fluid has a compression ratio of \(8 .\) The minimum and maximum temperatures in the cycle are 540 and 2400 R. Accounting for the variation of specific heats with temperature, determine ( \(a\) ) the amount of heat transferred to the air during the heat-addition process, \((b)\) the thermal efficiency, and \((c)\) the thermal efficiency of a Carnot cycle operating between the same temperature limits.
Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.
The compression ratio of an ideal dual cycle is 14. Air is at \(100 \mathrm{kPa}\) and \(300 \mathrm{K}\) at the beginning of the compression process and at \(2200 \mathrm{K}\) at the end of the heat-addition process. Heat transfer to air takes place partly at constant volume and partly at constant pressure, and it amounts to \(1520.4 \mathrm{kJ} / \mathrm{kg} .\) Assuming variable specific heats for air, determine \((a)\) the fraction of heat transferred at constant volume and \((b)\) the thermal efficiency of the cycle.
When we double the compression ratio of an ideal Otto cycle, what happens to the maximum gas temperature and pressure when the state of the air at the beginning of the compression and the amount of heat addition remain the same? Use constant specific heats at room temperature.
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