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- The maximum thermal efficiency possible for a power cycle operating between 1096°F and 267°F is _____. Express in four significant figures, not in percentage.1. A cooling tower has an efficiency of 65%. Water enters the tower at 55°C. The wet bulb temperature of surrounding air is 27°C. What is the temperature of water leaving the tower? a. 36.8°C b. 44.5°C c. 46.9°C d. 30.4°C 2. The change of temperature entering the cooling tower and wet bulb temperature of surrounding air is 25°C and efficiency is 65%. If mass of water leaving the tower is 10 kg/s, determine the heat carried by air. a. 720 kW b. 540 kW c. 680 kW d. 700 kW 3. The approach and efficiency of cooling tower is 10°C and 60%, respectively. If temperature of water leaving the tower is 37°C, what is the temperature of water entering? a. 46°C b. 52°C c. 68°C d. 48°C 4. A cooling tower is used to cool a jacket water loss from the engine. The heat generated by fuel is 2,500 kW and cooling loss is 30%. If temperature range of the tower is 15°C. Determine the mass flow of water entering the tower. a. 12 kg/s b. 14 kg/s c. 16 kg/s d. 18 kg/s3)A)What is radiation in Heat Transfer ? B)Does the radiation affect the lifetime of the turbine? C)How does the radiation affect the lifetime of the turbine?
- A power plant with a nominal rating of 1kW does not actually produce 1kW continuously because its capacity factor C - the fraction of the time that it is actually running at its rated power - is less than 100%. If the capacity factor C = 35%, how much energy will be generated by this power plant over 1 year in MJ?How do heat transfer and energy transformation affect heat engines in electricity production?20.The following performance of gas turbine engine: compressor inlet temperature, 525°R; compressor isentropic discharge temperature, 673°R; actual compressor discharge temperature, 693°R; turbine inlet temperature, 1505°R; turbine isentropic discharge temperature, 1185°R; and turbine actual discharge temperature, 1218°R. For these conditions calculate the turbine isentropic efficiency.A. 83.24% B. 89.68% C. 87.24% D. 92.68%
- An old gas turbine has an efficiency of 21 percent and develops a power output of 6000 kW. Determine the fuel consumption rate of this gas turbine, in L/min, if the fuel has a heating value of 42,000 kJ/kg and a density of 0.8 g/cm3 .A steam turbine is supplied with steam at 20.6 bar and 399°C. After the steam has expanded to 4.04 bar, it is reheated to 315.5°C and then expands down to a pressure of 0.065 bar. The efficiency of each expansion may take as 75%. 1. Determine the thermal efficiency, in percentile (%), of the cycle. 2. Determine the mass of steam required in kg per kW·hr.16. (a) Use energy-flow diagrams to show that the existence of a perfect heat engine would permit the construction of a perfect refrigerator, thus violating the Clausius statement of the second law. (b) Explain your answer briefly.
- The displacement volume of an internal combustion engine is 2.15 liters. The processes within each cylinder of the engine are modeled as an air-standard Diesel cycle with a cutoff ratio of 2.5. The state of the air at the beginning of compression is fixed by p1 = 1.6 bar, T1 = 325 K and V1 = 2.36 liters. If the cycle is executed 2100 times per min, determine:d) the power developed by the engine, in kW,e) and the thermal efficiency.A gas within a piston-cylinder assembly executes a Carnot power cycle during which the isothermal expansion occurs at TH = 500 K and the isothermal compression occurs at TC = 290 K. Determine: (a) the thermal efficiency. (b) the percent change in thermal efficiency if TH increases by 5% while TC remains the same. (c) the percent change in thermal efficiency if TC decreases by 5% while TH remains the same. (d) the percent change in thermal efficiency if TH increases by 5% and TC decreases by 5%.Identify valid processes as those that satisfy both the first and second laws of thermodynamics.