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Thermo_5th_Chap06_P069

Course: E 234, Spring 2008
School: Stevens
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Heat 6-18 Carnot Engines 6-69C No. 6-70C The one that has a source temperature of 600C. This is true because the higher the temperature at which heat is supplied to the working fluid of a heat engine, the higher the thermal efficiency. 6-71 The source and sink temperatures of a Carnot heat engine and the rate of heat supply are given. The thermal efficiency and the power output are to be determined. Assumptions...

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Heat 6-18 Carnot Engines 6-69C No. 6-70C The one that has a source temperature of 600C. This is true because the higher the temperature at which heat is supplied to the working fluid of a heat engine, the higher the thermal efficiency. 6-71 The source and sink temperatures of a Carnot heat engine and the rate of heat supply are given. The thermal efficiency and the power output are to be determined. Assumptions The Carnot heat engine operates steadily. Analysis (a) The thermal efficiency of a Carnot heat engine depends on the source and the sink temperatures only, and is determined from 300 K T 1000 K th,C = 1 - L = 1 - = 0.70 or 70% 1000 K TH 800 kJ/min (b) The power output of this heat engine is determined from the definition of thermal efficiency, & & W = Q = (0.70 )(800 kJ/min ) = 560 kJ/min = 9.33 kW net, out th H HE 300 K 6-72 The sink temperature of a Carnot heat engine and the rates of heat supply and heat rejection are given. The source temperature and the thermal efficiency of the engine are to be determined. Assumptions The Carnot heat engine operates steadily. Q Analysis (a) For reversible cyclic devices we have H Q L T = H rev TL source 650 kJ HE 250 kJ 24C Thus the temperature of the source TH must be Q 650 kJ TH = H TL = 250 kJ (297 K ) = 772.2 K Q L rev (b) The thermal efficiency of a Carnot heat engine depends on the source and the sink temperatures only, and is determined from 297 K T th,C = 1 - L = 1 - = 0.615 or 61.5% 772.2 K TH 6-73 [Also solved by EES on enclosed CD] The source and sink temperatures of a heat engine and the rate of heat supply are given. The maximum possible power output of this engine is to be determined. Assumptions The heat engine operates steadily. Analysis The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from 550C 298 K T th, max = th,C = 1 - L = 1 - = 0.638 or 63.8% 823 K TH 1200 kJ/min Then the maximum power output of this heat engine is determined from the definition of thermal efficiency to be & & W = Q = (0.638)(1200 kJ/min ) = 765.6 kJ/min = 12.8 kW net, out th H HE 25C 6-19 6-74 EES Problem 6-73 is reconsidered. The effects of the temperatures of the heat source and the heat sink on the power produced and the cycle thermal efficiency as the source temperature varies from 300C to 1000C and the sink temperature varies from 0C to 50C are to be studied. The power produced and the cycle efficiency against the source temperature for sink temperatures of 0C, 25C, and 50C are to be plotted. Analysis The problem is solved using EES, and the results are tabulated and plotted below. "Input Data from the Diagram Window" {T_H = 550 [C] T_L = 25 [C]} {Q_dot_H = 1200 [kJ/min]} "First Law applied to the heat engine" Q_dot_H - Q_dot_L- W_dot_net = 0 W_dot_net_KW=W_dot_net*convert(kJ/min,kW) "Cycle Thermal Efficiency - Temperatures must be absolute" eta_th = 1 - (T_L + 273)/(T_H + 273) "Definition of cycle efficiency" eta_th=W_dot_net / Q_dot_H th 0.52 0.59 0.65 0.69 0.72 0.75 0.77 0.79 TH [C] 300 400 500 600 700 800 900 1000 WnetkW [kW] 10.47 11.89 12.94 13.75 14.39 14.91 15.35 15.71 0.8 0.75 0.7 0.65 T = 50 C L = 25 C = 0C th 0.6 0.55 0.5 0.45 0.4 300 400 500 600 700 800 900 1000 Q H = 1200 kJ/m in T 20 18 16 14 12 H [C] T = 50 C L = 25 C = 0C W net,KW [kW ] 10 8 6 4 2 0 300 400 500 600 700 800 900 1000 Q H = 1200 kJ/m in T H [C] 6-20 6-75E The sink temperature of a Carnot heat engine, the rate of heat rejection, and the thermal efficiency are given. The power output of the engine and the source temperature are to be determined. Assumptions The Carnot heat engine operates steadily. Analysis (a) The rate of heat input to this heat engine is determined from the definition of thermal efficiency, & Q 800 Btu/min & th = 1 - & L 0.55 = 1 - QH = 1777.8 Btu/min & Q Q H H Then the power output of this heat engine can be determined from & & Wnet,out = th QH = (0.55)(1777.8 Btu/min ) = 977.8 Btu/min = 23.1 hp TH HE 800 Btu/min 60F (b) For reversible cyclic devices we have & QH Q & L T = H rev TL Thus the temperature of the source TH must be & Q 1777.8 Btu/min TH = H TL = 800 Btu/min (520 R ) = 1155.6 R Q & L rev 6-76 The source and sink temperatures of a OTEC (Ocean Thermal Energy Conversion) power plant are given. The maximum thermal efficiency is to be determined. Assumptions The power plant operates steadily. Analysis The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from 24C HE 3C W th, max = th,C = 1 - TL 276 K = 1- = 0.071 or 7.1% TH 297 K 6-77 The source and sink temperatures of a geothermal power plant are given. The maximum thermal efficiency is to be determined. Assumptions The power plant operates steadily. Analysis The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from 140C HE 20C W th, max = th,C = 1 - TL 20 + 273 K = 1- = 0.291 or 29.1% TH 140 + 273 K 6-21 6-78 An inventor claims to have developed a heat engine. The inventor reports temperature, heat transfer, and work output measurements. The claim is to be evaluated. Analysis The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from th, max = th,C = 1 - TL 290 K = 1- = 0.42 or 42% TH 500 K 500 K 700 kJ HE 290 K 300 kJ The actual thermal efficiency of the heat engine in question is th = Wnet 300 kJ = = 0.429 or 42.9% QH 700 kJ which is greater than the maximum possible thermal efficiency. Therefore, this heat engine is a PMM2 and the claim is false. 6-79E An inventor claims to have developed a heat engine. The inventor reports temperature, heat transfer, and work output measurements. The claim is to be evaluated. Analysis The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from th, max = th,C = 1 - TL 540 R = 1- = 0.40 or 40% TH 900 R 900 R 300 Btu HE 540 R 160 Btu The actual thermal efficiency of the heat engine in question is th = Wnet 160 Btu = = 0.533 or 53.3% QH 300 Btu which is greater than the maximum possible thermal efficiency. Therefore, this heat engine is a PMM2 and the claim is false. 6-22 6-80 A geothermal power plant uses geothermal liquid water at 160C at a specified rate as the heat source. The actual and maximum possible thermal efficiencies and the rate of heat rejected from this power plant are to be determined. Assumptions 1 The power plant operates steadily. 2 The kinetic and potential energy changes are zero. 3 Steam properties are used for geothermal water. Properties Using saturated liquid properties, the source and the sink state enthalpies of geothermal water are (Table A-4) Tsource = 160C hsource = 675.47 kJ/kg xsource = 0 Tsink = 25C hsink = 104.83 kJ/kg xsink = 0 Analysis (a) The rate of heat input to the plant may be taken as the enthalpy difference between the source and the sink for the power plant & & Qin = mgeo (hsource - hsink ) = (440 kg/s)(675.47 - 104.83) kJ/kg = 251,083 kW The actual thermal efficiency is th = & W net,out 22 MW = = 0.0876 = 8.8% & 251.083 MW Qin (b) The maximum thermal efficiency is the thermal efficiency of a reversible heat engine operating between the source and sink temperatures th, max = 1 - TL (25 + 273) K = 1- = 0.312 = 31.2% TH (160 + 273) K (c) Finally, the rate of heat rejection is & & & Qout = Qin - Wnet,out = 251.1 - 22 = 229.1 MW 6-23 Carnot Refrigerators and Heat Pumps 6-81C By increasing TL or by decreasing TH. 1 . TH / TL - 1 6-82C It is the COP that a Carnot refrigerator would have, COPR = 6-83C No. At best (when everything is reversible), the increase in the work produced will be equal to the work consumed by the refrigerator. In reality, the work consumed by the refrigerator will always be greater than the additional work produced, resulting in a decrease in the thermal efficiency of the power plant. 6-84C No. At best (when everything is reversible), the increase in the work produced will be equal to the work consumed by the refrigerator. In reality, the work consumed by the refrigerator will always be greater than the additional work produced, resulting in a decrease in the thermal efficiency of the power plant. 6-85C Bad idea. At best (when everything is reversible), the increase in the work produced will be equal to the work consumed by the heat pump. In reality, the work consumed by the heat pump will always be greater than the additional work produced, resulting in a decrease in the thermal efficiency of the power plant. 6-86 The refrigerated space and the environment temperatures of a Carnot refrigerator and the power consumption are given. The rate of heat removal from the refrigerated space is to be determined. Assumptions The Carnot refrigerator operates steadily. Analysis The coefficient of performance of a Carnot refrigerator depends on the temperature limits in the cycle only, and is determined from COPR, C = 1 1 = = 14.5 (TH / TL ) - 1 (22 + 273K )/(3 + 273K ) - 1 22C R 2 kW 3C The rate of heat removal from the refrigerated space is determined from the definition of the coefficient of performance of a refrigerator, & & QL = COPRWnet,in = (14.5)(2 kW ) = 29.0 kW = 1740 kJ/min 6-24 6-87 The refrigerated space and the environment temperatures for a refrigerator and the rate of heat removal from the refrigerated space are given. The minimum power input required is to be determined. Assumptions The refrigerator operates steadily. Analysis The power input to a refrigerator will be a minimum when the refrigerator operates in a reversible manner. The coefficient of performance of a reversible refrigerator depends on the temperature limits in the cycle only, and is determined from COPR, rev = 1 1 = = 8.03 (TH / TL ) - 1 (25 + 273 K )/ (- 8 + 273 K ) - 1 25C R 300 kJ/min -8C The power input to this refrigerator is determined from the definition of the coefficient of performance of a refrigerator, & QL 300 kJ/min & Wnet,in, min = = = 37.36 kJ/min = 0.623 kW COPR, max 8.03 6-88 The cooled space and the outdoors temperatures for a Carnot air-conditioner and the rate of heat removal from the air-conditioned room are given. The power input required is to be determined. Assumptions The air-conditioner operates steadily. Analysis The COP of a Carnot air conditioner (or Carnot refrigerator) depends on the temperature limits in the cycle only, and is determined from COPR, C = 1 1 = = 27.0 (TH / TL ) - 1 (35 + 273 K )/ (24 + 273 K ) - 1 35C A/C House 24C The power input to this refrigerator is determined from the definition of the coefficient of performance of a refrigerator, & QL 750 kJ/min & Wnet,in = = = 27.8 kJ/min = 0.463 kW COPR, max 27.0 6-89E The cooled space and the outdoors temperatures for an air-conditioner and the power consumption are given. The maximum rate of heat removal from the air-conditioned space is to be determined. Assumptions The air-conditioner operates steadily. Analysis The rate of heat removal from a house will be a maximum when the air-conditioning system operates in a reversible manner. The coefficient of performance of a reversible air-conditioner (or refrigerator) depends on the temperature limits in the cycle only, and is determined from COPR, rev = 1 1 = = 29.6 (TH / TL ) - 1 (90 + 460 R )/ (72 + 460 R ) - 1 90F The rate of heat removal from the house is determined from the definition of the coefficient of performance of a refrigerator, 42.41 Btu/min & & = 6277 Btu/min QL = COPRWnet,in = (29.6 )(5 hp ) 1 hp A/C House 72F 5 hp 6-25 6-90 The refrigerated space temperature, the COP, and the power input of a Carnot refrigerator are given. The rate of heat removal from the refrigerated space and its temperature are to be determined. Assumptions The refrigerator operates steadily. Analysis (a) The rate of heat removal from the refrigerated space is determined from the definition of the COP of a refrigerator, & & QL = COPRWnet,in = (4.5)(0.5 kW ) = 2.25 kW = 135 kJ/min 25C R TL 500 W COP = 4.5 (b) The temperature of the refrigerated space TL is determined from the coefficient of performance relation for a Carnot refrigerator, COPR, rev 1 1 = 4.5 = (TH / TL ) - 1 (25 + 273 K )/TL - 1 It yields TL = 243.8 K = -29.2C 6-91 An inventor claims to have developed a refrigerator. The inventor reports temperature and COP measurements. The claim is to be evaluated. Analysis The highest coefficient of performance a refrigerator can have when removing heat from a cool medium at -12C to a warmer medium at 25C is COPR, max = COPR, rev = (TH / TL ) - 1 (25 + 273 K )/ (- 12 + 273 K ) - 1 1 = 1 = 7.1 25C The COP claimed by the inventor is 6.5, which is below this maximum value, thus the claim is reasonable. However, it is not probable. R COP= 6.5 -12C 6-92 An experimentalist claims to have developed a refrigerator. The experimentalist reports temperature, heat transfer, and work input measurements. The claim is to be evaluated. Analysis The highest coefficient of performance a refrigerator can have when removing heat from a cool medium at -30C to a warmer medium at 25C is COPR, max = COPR, rev = (TH / TL ) - 1 (25 + 273 K )/ (- 30 + 273 K ) - 1 1 = 1 = 4.42 25C The work consumed the by actual refrigerator during this experiment is & Wnet,in = Wnet,in t = (2 kJ/s )(20 60 s ) = 2400 kJ R 2 kW 30,000 kJ -30C Then the coefficient of performance of this refrigerator becomes COPR = QL 30,000kJ = = 12.5 Wnet,in 2400kJ which is above the maximum value. Therefore, these measurements are not reasonable. 6-26 6-93E An air-conditioning system maintains a house at a specified temperature. The rate of heat gain of the house and the rate of internal heat generation are given. The maximum power input required is to be determined. Assumptions The air-conditioner operates steadily. Analysis The power input to an air-conditioning system will be a minimum when the air-conditioner operates in a reversible manner. The coefficient of performance of a reversible air-conditioner (or refrigerator) depends on the temperature limits in the cycle only, and is determined from COPR, rev = 1 1 = = 26.75 (TH / TL ) - 1 (95 + 460 R )/ (75 + 460 R ) - 1 95F A/C 800 kJ/min House 75F The cooling load of this air-conditioning system is the sum of the heat gain from the outside and the heat generated within the house, & Q L = 800 + 100 = 900 Btu/min The power input to this refrigerator is determined from the definition of the coefficient of performance of a refrigerator, & 900 Btu/min QL & = = 33.6 Btu/min = 0.79 hp Wnet,in, min = COPR, max 26.75 6-94 A heat pump maintains a house at a specified temperature. The rate of heat loss of the house is given. The minimum power input required is to be determined. Assumptions The heat pump operates steadily. Analysis The power input to a heat pump will be a minimum when the heat pump operates in a reversible manner. The COP of a reversible heat pump depends on the temperature limits in the cycle only, and is determined from COPHP, rev = 1 1 = = 10.2 1 - (TL / TH ) 1 - (- 5 + 273 K )/ (24 + 273 K ) 80,000 kJ/h House 24C The required power input to this reversible heat pump is determined from the definition of the coefficient of performance to be & Wnet,in, min = & 80,000 kJ/h 1 h QH = 3600 s = 2.18 kW COPHP 10.2 HP -5C which is the minimum power input required. 6-27 6-95 A heat pump maintains a house at a specified temperature. The rate of heat loss of the house and the power consumption of the heat pump are given. It is to be determined if this heat pump can do the job. Assumptions The heat pump operates steadily. Analysis The power input to a heat pump will be a minimum when the heat pump operates in a reversible manner. The coefficient of performance of a reversible heat pump depends on the temperature limits in the cycle only, and is determined from COPHP, rev = 1 1 = = 14.75 1 - (TL / TH ) 1 - (2 + 273 K )/ (22 + 273 K ) 110,000 kJ/h The required power input to this reversible heat pump is determined from the definition of the coefficient of performance to be & Wnet,in, min = & 110,000 kJ/h 1 h QH = 3600 s = 2.07 kW COPHP 14.75 House 22C HP 5 kW This heat pump is powerful enough since 5 kW > 2.07 kW. 6-96 A heat pump that consumes 5-kW of power when operating maintains a house at a specified temperature. The house is losing heat in proportion to the temperature difference between the indoors and the outdoors. The lowest outdoor temperature for which this heat pump can do the job is to be determined. Assumptions The heat pump operates steadily. Analysis Denoting the outdoor temperature by TL, the heating load of this house can be expressed as & QH = (5400 kJ/h K )(294 - TL ) = (1.5 kW/K )(294 - TL )K The coefficient of performance of a Carnot heat pump depends on the temperature limits in the cycle only, and can be expressed as COPHP = 1 1 = 1 - (TL / TH ) 1 - TL /(294 K) & QH & W 5400 kJ/h.K House 21C or, as COPHP = = (1.5 kW/K )(294 - TL )K 6 kW HP TL 6 kW net,in Equating the two relations above and solving for TL, we obtain TL = 259.7 K = -13.3C 6-28 6-97 A heat pump maintains a house at a specified temperature in winter. The maximum COPs of the heat pump for different outdoor temperatures are to be determined. Analysis The coefficient of performance of a heat pump will be a maximum when the heat pump operates in a reversible manner. The coefficient of performance of a reversible heat pump depends on the temperature limits in the cycle only, and is determined for all three cases above to be COPHP ,rev = COPHP ,rev = COPHP ,rev = 1 - (T L / T H ) 1 = 1 = 29.3 1 - (10 + 273K )/ (20 + 273K ) 20C HP TL 1 1 = = 11.7 1 - (T L / T H ) 1 - (- 5 + 273K )/ (20 + 273K ) 1 - (T L / T H ) 1 = 1 = 5.86 1 - (- 30 + 273K )/ (20 + 273K ) 6-98E A heat pump maintains a house at a specified temperature. The rate of heat loss of the house is given. The minimum power inputs required for different source temperatures are to be determined. Assumptions The heat pump operates steadily. Analysis (a) The power input to a heat pump will be a minimum when the heat pump operates in a reversible manner. If the outdoor air at 25F is used as the heat source, the COP of the heat pump and the required power input are determined to be COPHP, max = COPHP, rev = 1 1 = = 10.15 1 - (TL / TH ) 1 - (25 + 460 R )/ (78 + 460 R ) 55,000 Btu/h and & Wnet,in, min = & 55,000 Btu/h 1 hp QH = 2545 Btu/h = 2.13 hp COPHP, max 10.15 House 78F (b) If the well-water at 50F is used as the heat source, the COP of the heat pump and the required power input are determined to be COPHP, max = COPHP, rev = 1 1 = = 19.2 1 - (TL / TH ) 1 - (50 + 460 R )/ (78 + 460 R ) HP 25F or 50F and & Wnet,in, min = & 55,000 Btu/h 1 hp QH = 2545 Btu/h = 1.13 hp COPHP, max 19.2 6-29 6-99 A Carnot heat pump consumes 8-kW of power when operating, and maintains a house at a specified temperature. The average rate of heat loss of the house in a particular day is given. The actual running time of the heat pump that day, the heating cost, and the cost if resistance heating is used instead are to be determined. Analysis (a) The coefficient of performance of this Carnot heat pump depends on the temperature limits in the cycle only, and is determined from COPHP, rev = 1 1 = = 16.3 1 - (TL / TH ) 1 - (2 + 273 K )/ (20 + 273 K ) House 20C 82,000 kJ/h The amount of heat the house lost that day is & QH = QH (1 day ) = (82,000 kJ/h )(24 h ) = 1,968,000 kJ Then the required work input to this Carnot heat pump is determined from the definition of the coefficient of performance to be Wnet,in = 1,968,000 kJ QH = = 120,736 kJ COPHP 16.3 HP 8 kW Thus the length of time the heat pump ran that day is t = Wnet,in 120,736 kJ = = 15,092 s = 4.19 h & W 8 kJ/s net,in 2C (b) The total heating cost that day is & Cost = W price = Wnet,in t (price ) = (8 kW )(4.19 h )(0.085 $/kWh ) = $2.85 ( ) (c) If resistance heating were used, the entire heating load for that day would have to be met by electrical energy. Therefore, the heating system would consume 1,968,000 kJ of electricity that would cost 1 kWh New Cost = QH price = (1,968,000kJ ) 3600 kJ (0.085 $/kWh ) = $46.47 6-30 6-100 A Carnot heat engine is used to drive a Carnot refrigerator. The maximum rate of heat removal from the refrigerated space and the total rate of heat rejection to the ambient air are to be determined. Assumptions The heat engine and the refrigerator operate steadily. Analysis (a) The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from th, max = th,C = 1 - TL 300 K = 1- = 0.744 TH 1173 K 900C 800 kJ/min -5C Then the maximum power output of this heat engine is determined from the definition of thermal efficiency to be & & Wnet,out = th QH = (0.744 )(800 kJ/min ) = 595.2 kJ/min & which is also the power input to the refrigerator, Wnet,in . HE R 27C The rate of heat removal from the refrigerated space will be a maximum if a Carnot refrigerator is used. The COP of the Carnot refrigerator is COPR, rev = 1 1 = = 8.37 (TH / TL ) - 1 (27 + 273 K )/ (- 5 + 273 K ) - 1 Then the rate of heat removal from the refrigerated space becomes & & QL , R = COPR, rev Wnet,in = (8.37 )(595.2 kJ/min ) = 4982 kJ/min ( )( ) (b) The total rate of heat rejection to the ambient air is the sum of the heat rejected by the heat engine & & ( QL , HE ) and the heat discarded by the refrigerator ( QH , R ), & & & QL , HE = QH , HE - Wnet,out = 800 - 595.2 = 204.8 kJ/min & & & QH , R = QL , R + Wnet,in = 4982 + 595.2 = 5577.2 kJ/min and & & & Qambient = QL, HE + QH , R = 204.8 + 5577.2 = 5782 kJ/min 6-31 6-101E A Carnot heat engine is used to drive a Carnot refrigerator. The maximum rate of heat removal from the refrigerated space and the total rate of heat rejection to the ambient air are to be determined. Assumptions The heat engine and the refrigerator operate steadily. Analysis (a) The highest thermal efficiency a heat engine operating between two specified temperature limits can have is the Carnot efficiency, which is determined from th, max = th,C = 1 - TL 540 R = 1- = 0.75 TH 2160 R 1700F 700 Btu/min HE 80F 20F Then the maximum power output of this heat engine is determined from the definition of thermal efficiency to be & & Wnet,out = th QH = (0.75)(700 Btu/min ) = 525 Btu/min & which is also the power input to the refrigerator, Wnet,in . R The rate of heat removal from the refrigerated space will be a maximum if a Carnot refrigerator is used. The COP of the Carnot refrigerator is COPR, rev = 1 1 = = 8.0 (TH / TL ) - 1 (80 + 460 R )/ (20 + 460 R ) - 1 Then the rate of heat removal from the refrigerated space becomes & & QL , R = COPR, rev Wnet,in = (8.0 )(525 Btu/min ) = 4200 Btu/min ( )( ) (b) The total rate of heat rejection to the ambient air is the sum of the heat rejected by the heat engine & & ( QL , HE ) and the heat discarded by the refrigerator ( QH , R ), & & & QL , HE = QH , HE - Wnet,out = 700 - 525 = 175 Btu/min & & & QH , R = QL , R + Wnet,in = 4200 + 525 = 4725 Btu/min and & & & Qambient = QL , HE + QH , R = 175 + 4725 = 4900 Btu/min 6-32 6-102 A commercial refrigerator with R-134a as the working fluid is considered. The condenser inlet and exit states are specified. The mass flow rate of the refrigerant, the refrigeration load, the COP, and the minimum power input to the compressor are to be determined. Assumptions 1 The refrigerator operates steadily. 2 The kinetic and potential energy changes are zero. Properties The properties of R-134a and water are (Steam and R-134a tables) P = 1.2 MPa 1 h1 = 278.27 kJ/kg T1 = 50C T2 = Tsat@1.2 MPa + Tsubcool = 46.3 - 5 = 41.3C P2 = 1.2 MPa h2 = 110.17 kJ/kg T2 = 41.3C Tw,1 = 18C hw,1 = 75.54 kJ/kg x w,1 = 0 Tw, 2 = 26C hw, 2 = 109.01 kJ/kg x w, 2 = 0 26C 1.2 MPa 5C subcool QH Condenser Water 18C 1.2 MPa 50C Expansion valve Win Compressor Evaporator QL Analysis (a) The rate of heat transferred to the water is the energy change of the water from inlet to exit & & Q H = m w (hw, 2 - hw,1 ) = (0.25 kg/s)(109.01 - 75.54) kJ/kg = 8.367 kW The energy decrease of the refrigerant is equal to the energy increase of the water in the condenser. That is, & & Q H = m R (h1 - h2 ) m R = & & QH 8.367 kW = = 0.0498 kg/s h1 - h2 (278.27 - 110.17) kJ/kg (b) The refrigeration load is & & & Q L = Q H - Win = 8.37 - 3.30 = 5.07 kW (c) The COP of the refrigerator is determined from its definition, COP = & Q L 5.07 kW = = 1.54 & 3.3 kW Win 1 1 = = 4.49 TH / TL - 1 (18 + 273) /(-35 + 273) - 1 (d) The COP of a reversible refrigerator operating between the same temperature limits is COPmax = Then, the minimum power input to the compressor for the same refrigeration load would be & Win, min = & QL 5.07 kW = = 1.13 kW COPmax 4.49 6-33 6-103 An air-conditioner with R-134a as the working fluid is considered. The compressor inlet and exit states are specified. The actual and maximum COPs and the minimum volume flow rate of the refrigerant at the compressor inlet are to be determined. Assumptions 1 The air-conditioner operates steadily. 2 The kinetic and potential energy changes are zero. Properties The properties of R-134a at the compressor inlet and exit states are (Tables A-11 through A-13) P1 = 500 kPa h1 = 259.30 kJ/kg 3 x1 = 1 v1 = 0.04112 m /kg P2 = 1.2 MPa h2 = 278.27 kJ/kg T2 = 50C QH Condenser Expansion valve 1.2 MPa 50C Win Compressor 500 kPa sat. vap. Analysis (a) The mass flow rate of the refrigerant and the power consumption of the compressor are 1 m 3 1 min 100 L/min 1000 L 60 s & V1 & mR = = = 0.04053 kg/s 3 v1 0.04112 m /kg Evaporator QL & & Win = m R (h2 - h1 ) = (0.04053 kg/s)(278.27 - 259.30) kJ/kg = 0.7686 kW The heat gains to the room must be rejected by the air-conditioner. That is, 1 min & & & Q L = Q heat + Qequipment = (250 kJ/min) + 0.9 kW = 5.067 kW 60 s Then, the actual COP becomes COP = & QL 5.067 kW = = 6.59 & Win 0.7686 kW 1 1 = = 37.4 T H / T L - 1 (34 + 273) /(26 + 273) - 1 & QL 5.067 kW = = 0.1356 kW COPmax 37.38 (b) The COP of a reversible refrigerator operating between the same temperature limits is COPmax (c) The minimum power input to the compressor for the same refrigeration load would be & Win, min = The minimum mass flow rate is & Win, min 0.1356 kW & mR, min = = = 0.007149 kg/s h2 - h1 (278.27 - 259.30) kJ/kg Finally, the minimum volume flow rate at the compressor inlet is & V&min,1 = mR, minv 1 = (0.007149 kg/s)(0.04112 m 3 /kg) = 0.000294 m 3 /s = 17.64 L/min
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Stevens - E - 234
6-34Special Topic: Household Refrigerators 6-104C It is a bad idea to overdesign the refrigeration system of a supermarket so that the entire airconditioning needs of the store can be met by refrigerated air without installing any air-conditioning
Stevens - E - 234
7-1Chapter 7 ENTROPYEntropy and the Increase of Entropy Principle 7-1C Yes. Because we used the relation (QH/TH) = (QL/TL) in the proof, which is the defining relation of absolute temperature. 7-2C No. The Q represents the net heat transfer dur
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7-26Entropy Change of Incompressible Substances 7-52C No, because entropy is not a conserved property.7-53 A hot copper block is dropped into water in an insulated tank. The final equilibrium temperature of the tank and the total entropy change a
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7-51Reversible Steady-Flow Work 7-87C The work associated with steady-flow devices is proportional to the specific volume of the gas. Cooling a gas during compression will reduce its specific volume, and thus the power consumed by the compressor. 7
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7-51Reversible Steady-Flow Work 7-87C The work associated with steady-flow devices is proportional to the specific volume of the gas. Cooling a gas during compression will reduce its specific volume, and thus the power consumed by the compressor. 7
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7-107Special Topic: Reducing the Cost of Compressed Air7-150 The total installed power of compressed air systems in the US is estimated to be about 20 million horsepower. The amount of energy and money that will be saved per year if the energy co
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7-1357-184 The validity of the Clausius inequality is to be demonstrated using a reversible and an irreversible heat engine operating between the same temperature limits. Analysis Consider two heat engines, one reversible and one irreversible, both
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7-1487-198 Refrigerant-134a is vaporized by air in the evaporator of an air-conditioner. For specified flow rates, the exit temperature of air and the rate of entropy generation are to be determined for the cases of an insulated and uninsulated eva
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8-1Chapter 8 EXERGY A MEASURE OF WORK POTENTIALExergy, Irreversibility, Reversible Work, and Second-Law Efficiency 8-1C Reversible work differs from the useful work by irreversibilities. For reversible processes both are identical. Wu = Wrev -I.
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8-33Second-Law Analysis of Control Volumes8-54 Steam is throttled from a specified state to a specified pressure. The wasted work potential during this throttling process is to be determined. Assumptions 1 This is a steady-flow process since ther
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8-608-79 A rigid tank initially contains saturated R-134a vapor. The tank is connected to a supply line, and R134a is allowed to enter the tank. The mass of the R-134a that entered the tank and the exergy destroyed during this process are to be det
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8-79Review Problems8-95 Refrigerant-134a is expanded adiabatically in an expansion valve. The work potential of R-134a at the inlet, the exergy destruction, and the second-law efficiency are to be determined. Assumptions 1 Steady operating condit
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8-968-113 A well-insulated room is heated by a steam radiator, and the warm air is distributed by a fan. The average temperature in the room after 30 min, the entropy changes of steam and air, and the exergy destruction during this process are to b
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8-1118-124 An evacuated bottle is surrounded by atmospheric air. A valve is opened, and air is allowed to fill the bottle. The amount of heat transfer through the wall of the bottle when thermal and mechanical equilibrium is established and the amo
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9-1Chapter 9 GAS POWER CYCLESActual and Ideal Cycles, Carnot cycle, Air-Standard Assumptions 9-1C The Carnot cycle is not suitable as an ideal cycle for all power producing devices because it cannot be approximated using the hardware of actual pow
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9-40Stirling and Ericsson Cycles 9-60C The efficiencies of the Carnot and the Stirling cycles would be the same, the efficiency of the Otto cycle would be less. 9-61C The efficiencies of the Carnot and the Ericsson cycles would be the same, the eff
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9-70Brayton Cycle with Intercooling, Reheating, and Regeneration 9-101C As the number of compression and expansion stages are increased and regeneration is employed, the ideal Brayton cycle will approach the Ericsson cycle. 9-102C (a) decrease, (b)
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9-97Review Problems9-132 A turbocharged four-stroke V-16 diesel engine produces 3500 hp at 1200 rpm. The amount of power produced per cylinder per mechanical and per thermodynamic cycle is to be determined. Analysis Noting that there are 16 cylin
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9-1319-159 EES The effect of variable specific heats on the thermal efficiency of the ideal Otto cycle using air as the working fluid is to be investigated. The percentage of error involved in using constant specific heat values at room temperature
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10-1Chapter 10 VAPOR AND COMBINED POWER CYCLESCarnot Vapor Cycle 10-1C Because excessive moisture in steam causes erosion on the turbine blades. The highest moisture content allowed is about 10%. 10-2C The Carnot cycle is not a realistic model for
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10-3010-46 A steam power plant operates on an ideal regenerative Rankine cycle with two open feedwater heaters. The net power output of the power plant and the thermal efficiency of the cycle are to be determined. Assumptions 1 Steady operating con
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10-5210-67 A cogeneration plant is to generate power and process heat. Part of the steam extracted from the turbine at a relatively high pressure is used for process heating. The net power produced and the utilization factor of the plant are to be
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10-77Special Topic: Binary Vapor Cycles 10-82C Binary power cycle is a cycle which is actually a combination of two cycles; one in the high temperature region, and the other in the low temperature region. Its purpose is to increase thermal efficien
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10-9310-99 A combined gas-steam power plant is considered. The topping cycle is an ideal gas-turbine cycle and the bottoming cycle is an ideal reheat Rankine cycle. The mass flow rate of air in the gas-turbine cycle, the rate of total heat input, a
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11-1Chapter 11 REFRIGERATION CYCLESThe Reversed Carnot Cycle 11-1C Because the compression process involves the compression of a liquid-vapor mixture which requires a compressor that will handle two phases, and the expansion process involves the e
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11-36Gas Refrigeration Cycles 11-49C The ideal gas refrigeration cycle is identical to the Brayton cycle, except it operates in the reversed direction. 11-50C The reversed Stirling cycle is identical to the Stirling cycle, except it operates in the
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12-1Chapter 12 THERMODYNAMIC PROPERTY RELATIONSPartial Derivatives and Associated Relations 12-1Czdzx dx(z)y (z)xy dy dz = (z ) x + (z ) yy x dx x +dx dyy + dyyx12-2C For functions that depend on one variable, they are identical
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12-2912-58E The enthalpy of nitrogen at 400 R and 2000 psia is to be determined using data from the ideal-gas nitrogen table and the generalized enthalpy departure chart. Analysis (a) From the ideal gas table of nitrogen (Table A-18E) we readh = 2
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13-1Chapter 13 GAS MIXTURESComposition of Gas Mixtures 13-1C It is the average or the equivalent gas constant of the gas mixture. No. 13-2C No. We can do this only when each gas has the same mole fraction. 13-3C It is the average or the equivalent
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13-3513-64 Heat is transferred to a gas mixture contained in a piston cylinder device discussed in previous problem. The total entropy change and the exergy destruction are to be determined for two cases. Analysis The entropy generated during this
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14-1Chapter 14 GAS-VAPOR MIXTURES AND AIR CONDITIONINGDry and Atmospheric Air, Specific and Relative Humidity 14-1C Yes; by cooling the air at constant pressure. 14-2C Yes. 14-3C Specific humidity will decrease but relative humidity will increase.
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14-2014-69E Air enters a heating section at a specified pressure, temperature, velocity, and relative humidity. The exit temperature of air, the exit relative humidity, and the exit velocity are to be determined. Assumptions 1 This is a steady-flow
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14-45Adiabatic Mixing of Airstreams 14-100C This will occur when the straight line connecting the states of the two streams on the psychrometric chart crosses the saturation line. 14-101C Yes.14-102 Two airstreams are mixed steadily. The specific
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14-58Review Problems14-115 Air is compressed by a compressor and then cooled to the ambient temperature at high pressure. It is to be determined if there will be any condensation in the compressed air lines. Assumptions The air and the water vapo
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15-1Chapter 15 CHEMICAL REACTIONSFuels and Combustion 15-1C Gasoline is C8H18, diesel fuel is C12H26, and natural gas is CH4. 15-2C Nitrogen, in general, does not react with other chemical species during a combustion process but its presence affec
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15-24First Law Analysis of Reacting Systems 15-46C In this case U + Wb = H, and the conservation of energy relation reduces to the form of the steady-flow energy relation. 15-47C The heat transfer will be the same for all cases. The excess oxygen a
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15-43Adiabatic Flame Temperature 15-68C For the case of stoichiometric amount of pure oxygen since we have the same amount of chemical energy released but a smaller amount of mass to absorb it. 15-69C Under the conditions of complete combustion wit
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15-64Review Problems15-88 A sample of a certain fluid is burned in a bomb calorimeter. The heating value of the fuel is to be determined. Properties The specific heat of water is 4.18 kJ/kg.C (Table A-3). Analysis We take the water as the system,
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15-8315-102 A mixture of 40% by volume methane, CH4, and 60% by volume propane, C3H8, is burned completely with theoretical air. The amount of water formed during combustion process that will be condensed is to be determined. 40% CH4 Assumptions 1
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16-1Chapter 16 CHEMICAL AND PHASE EQUILIBRIUMThe Kp and Equilibrium Composition of Ideal Gases 16-1C Because when a reacting system involves heat transfer, the increase-in-entropy principle relation requires a knowledge of heat transfer between th
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16-1716-29E A mixture of CO, O2, and N2 is heated to a high temperature at a constant pressure. The equilibrium composition is to be determined. Assumptions 1 The equilibrium composition consists of CO2, CO, O2, and N2. 2 The constituents of the mi
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16-4316-52 The KP value of the combustion process H2 + 1/2O2 H2O is to be determined at a specified temperature using hR data and KP value . Assumptions Both the reactants and products are ideal gases. Analysis The hR and KP data are related to ea
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16-6016-83 A mixture of H2 and O2 in a tank is ignited. The equilibrium composition of the product gases and the amount of heat transfer from the combustion chamber are to be determined. Assumptions 1 The equilibrium composition consists of H2O, H2
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17-1Chapter 17 COMPRESSIBLE FLOWStagnation Properties 17-1C The temperature of the air will rise as it approaches the nozzle because of the stagnation process. 17-2C Stagnation enthalpy combines the ordinary enthalpy and the kinetic energy of a fl
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17-45Duct Flow with Heat Transfer and Negligible Friction (Rayleigh Flow) 17-96C The characteristic aspect of Rayleigh flow is its involvement of heat transfer. The main assumptions associated with Rayleigh flow are: the flow is steady, one-dimensi
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17-64Review Problems 17-118 A leak develops in an automobile tire as a result of an accident. The initial mass flow rate of air through the leak is to be determined. Assumptions 1 Air is an ideal gas with constant specific heats. 2 Flow of air thro
Columbia - MATH - 1201
Columbia - MATH - 1201
Columbia - MATH - 1201
Columbia - MATH - 1201
Columbia - MATH - 1201
MS Mary - MATH - 348
Name Mathematics 364 Extra Credit 1 (Due Monday 3/10/08)Directions: To get the full 5 points, the problems must be all correct or nearly so. Most are short and easy to do. Feel free to ask questions on any of the problems. 1 3 4 3 5 . 1. (a) Find
USC - JS - 211g
Is Reconcination Possible After Genocide?: The Case of RwandaMARK R. AMSTUTZFrom April to July 1994, Rwanda experienced one of the most destructive mass atrocities in history, resulting in the death of some 800,000 persons. The genocide began on 6
Maryland - MATH - 141
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Maryland - PHYS - 161,260,27
CHAPTER14Oscillations1* Deezo the Clown slept in again. As he roller-skates out the door at breakneck speed on his way to a lunchtime birthday party, his superelastic suspenders catch on a fence post, and he flies back and forth, oscillating w
Maryland - MATH - 241
Maryland - PHYS - 260
Lecture 5 (Feb. 6) Pressure in liquids and gases Measuring and using pressure Archimedes' principle (float or sink?)master formulaPressurep= F A (SI units: 1 N/m2 1 P a) Measuring device: fluid pushes against(like tension in string)"spr
Maryland - PHYS - 260
Lecture 21 heat engines and refrigerators using idealgas as working substance Brayton cycleIdeal gas Heat Enginesclosed cycle trajectory: clockwise for Wout > 0 Wout = Wexpand - |Wcompress | = area inside closed curveIdeal gas summary I
Maryland - PHYS - 161,260,27
CHAPTER21Thermal Properties and Processes1* 2 Why does the mercury level first decrease slightly when a thermometer is placed in warm water? A large sheet of metal has a hole cut in the middle of it. When the sheet is heated, the area of the
Maryland - PHYS - 161
Maryland - PHYS - 161,260,27
CHAPTER Magnetic Induction301* A uniform magnetic field of magnitude 2000 G is parallel to the x axis. A square coil of side 5 cm has a single turn and makes an angle with the z axis as shown in Figure 30-28. Find the magnetic flux through the