Chapter 9: Problem 27
How is the rpm (revolutions per minute) of an actual four-stroke gasoline engine related to the number of thermodynamic cycles? What would your answer be for a two-stroke engine?
Chapter 9: Problem 27
How is the rpm (revolutions per minute) of an actual four-stroke gasoline engine related to the number of thermodynamic cycles? What would your answer be for a two-stroke engine?
All the tools & learning materials you need for study success - in one app.
Get started for freeAn 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.
An Otto cycle with air as the working fluid has a compression ratio of \(10.4 .\) Under cold-air-standard conditions, the thermal efficiency of this cycle is \((a) 10\) percent (b) 39 percent \((c) 61\) percent \((d) 79\) percent \((e) 82\) percent
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.
A four-stroke turbocharged \(V-16\) diesel engine built by GE Transportation Systems to power fast trains produces 4400 hp at 1500 rpm. Determine the amount of work produced per cylinder per ( \(a\) ) mechanical cycle and ( \(b\) ) thermodynamic cycle.
Exhaust gases from the turbine of a simple Brayton cycle are quite hot and may be used for other thermal purposes. One proposed use is generating saturated steam at \(110^{\circ} \mathrm{C}\) from water at \(30^{\circ} \mathrm{C}\) in a boiler. This steam will be distributed to several buildings on a college campus for space heating. A Brayton cycle with a pressure ratio of 6 is to be used for this purpose. Plot the power produced, the flow rate of produced steam, and the maximum cycle temperature as functions of the rate at which heat is added to the cycle. The temperature at the turbine inlet is not to exceed \(2000^{\circ} \mathrm{C}\)
What do you think about this solution?
We value your feedback to improve our textbook solutions.