Chapter 2 Solutions. 2.1 (D) Pressure and temperature are dependent during phase change and independent when in a single phase.

Size: px
Start display at page:

Download "Chapter 2 Solutions. 2.1 (D) Pressure and temperature are dependent during phase change and independent when in a single phase."

Transcription

1 Chater Solutions.1 (D) Pressure and temerature are deendent during hase change and indeendent when in a single hase.. (B) Sublimation is the direct conversion of a solid to a gas. To observe this rocess, set a iece of dry ice out on a table to.. (B) From Table B-1 at 9000 m, the atmosheric ressure is 0% of atmosheric ressure at sea level which is 0 kpa. From Table C- the saturation temerature for 0 kpa or 0.0 MPa is 69.1ºC..4 (A) The water is subcooled. If it were saturated it would be at 100ºC (1ºF) and cook you..5 (A) From Table C-1 at 00 C and v = 0.00 m /kg, the water is a saturated mixture. At 00ºC and v = 0. m /kg the water is a suerheated vaor. Grah (A) describes this rocess. Constant ressure goes u to the right and constant temerature goes down to the right..6 (D) The mass is kg and the volume is 0.08 m. The secific volume is 0.08 m v = = 0.04 m /kg kg From Table C-1 we get v f = m /kg and v g = m /kg. Calculating the quality we get v vf x = = = 0.1 v v g f.7 (A) From Table C- for P = 10 MPa and T = 00 C, the water is subcooled since saturation temerature at 10 MPa is 11 C. This means that the secific volume is v f at 00 C. From Table C-1 we get vf = m / kg. V = 0 kg m /kg = 0.08 m.8 (C) The secific volume at 400 C and 4 MPa is v 1 = m /kg = v. The volume doesn t change if it is rigid. Either Table C-1 or C- will contain the desired ressure. Table C-1 is referred since the v-entries are closer together. The entry at 0 C is v 1 = 0.07 m /kg, quite close to 0.07 m /kg. Interolation need not be accurate in order to select the correct answer: P.8 MPa..9 (A) (1000 liters = 1 m ) V = L = 0.00 m. Remember that quality is calculated on a mass basis, not a volume basis. From Table C-1 for a temerature of 00 C we get v f = m /kg and v g = m /kg. The liquid mass = V liquid /v f = m / m /kg = kg. The vaor mass = V vaor /v g = 0.00 m /0.174 m /kg = kg. Now we can calculate the quality: mvaor kg x = = = = 1.8% m kg kg total 9

2 .10 (B) Average the h-values between 6 MPa and 7 MPa for 600 C and 700 C in Table C-. There is only a small change in enthaly with ressure so a calculator is not needed: At 600 C: h= 654 At 700 C: h= Now, interolate between 654 and 891: h = ( ) = 8 kj/kg 4.11 (A) The tire is a torus with a minor radius r of 0.01 m and a major radius R of 1 m. The volume of the tire is the circumference times the area of the tire: 4 V = πd A= π 1 ( π 0.01 ) = m Treat air as an ideal gas (to check the units, use kpa = kn/m and kj = kn m): 4 ( 500 kpa)( m ) PV m = = = kg RT kj 0.87 ( 9 K) kg K.1 (C) The ressure in the cylinder can be found using the ideal gas law: mrt P = = = 18 kpa or 8 kpa gage V π The ressure balances the weight of the iston but we must use the gage ressure or add a force on the to of the iston due to the atmosheric ressure: W = PA = π 0.15 = 4070 N.1 (A) Because the temerature is so low and the ressure quite high, we anticiate non-ideal gas behavior. So, let s aroximate the Z-factor using Aendix G: P T 10 PR = 0.80, TR Z 0.59 P =.77 = = T = 1 = = cr PV m = = =.7 kg ZRT P (B) For an ideal gas ρ = =. ρ = = kg/m outside v RT ρ = = kg/m inside Difference = = 0.4 kg/m cr 10

3 Δh (B) C = = =.8 kj/kg C using a central-difference ΔT aroximation. Comare with the value from Table B- where steam is treated as an ideal gas (near atmosheric temerature and low ressure)..16 (D) From Table B-: C = 1.87 kj/kg K. Δ h= C Δ T = = kj/kg P From Table C- h 00 = kj/kg and h 600 = 704 kj/kg Δ h = = 8.5 kj/kg %difference = 100% = 10% (A) The enthaly change to warm u the ice is found by aroximating C to be.05 kj/kg C between 0 C and 0 C (see Table B-4): Δ Hice = mδ h= = 410 kj The ice is now at 0 C at which state it melts, requiring the heat of fusion, 0 kj/kg: Δ Hmelt = mδ hfusion = 10 0 = 00 kj If the temerature of the water is now raised from 0 C to 100 C, the enthaly change is found using C = 4.18 kj/kg C to be Δ Hmelt = mδ hwater = mcδ T = = 4180 kj Finally, the steam is suerheated to 00 C. From Table C- at P = 0.1 MPa, we find Δ H = mδ h= 10 ( ) = 1998 kj The total enthaly change to warm the ice, melt the ice, vaorize the water, and suerheat the steam is Δ H = = 990 kj.18 a) From Table C-1 for T = 140 C, P sat = 0.61 MPa = 61 kpa b) For T = 00 C, P sat = MPa = 1554 kpa c) For T = 0 C, P sat = 11.7 MPa = kpa.19 a) From Table C-E for P = 1 sia, T sat is calculated by interolating between 10 sia and 14.7 sia: T = 1 sia 10 sia sat T sat = 01. F sia 10 sia b) For P = 8 sia, interolate between 5 sia and 0 sia: o T sat 8 sia 5 sia = 0 sia 5 sia o o T sat = 46. F 11

4 c) For P = 50 sia, T sat = 81.0 F.0 For a temerature of 90 C, we use Table C-1 to find P sat = MPa = 70.1 kpa. From Table B-1 we see that P/P 0 = between 000 m and 000 m of altitude. We interolate to find the exact altitude h: h 000 m = 000 m 000 m h = 880 m.1 We use Table C-1E to find the ressure and Table C-E to find the corresonding saturation temerature. a) For h = 1,000 ft we get P/P 0 by interolating between 10,000 ft and 15,000 ft. P P ,000 ft 10,000 ft =. P/P 0 = ,000 ft 10,000 ft P = sia = 9.4 sia For this ressure we get the saturation temerature by interolation between 8 sia and 10 sia: T sat 9.4 sia 8 sia =. T sat = 190 o F sia 8 sia b) For h = 0,000 ft we get P/P 0 = 0.46 so P = sia = 6.8 sia. We have to interolate between 6 and 8 sia to find the saturation temerature: T sat 6.8 sia 6 sia =. T sat = 175. o F sia 6 sia c) For h =,000 ft we have to interolate between 0,000 ft and 5,000 ft to get P/P 0. P P ,000 ft 0,000 ft =. P/P o = 0.7 and P = sia = 4 sia , 000 ft 0, 000 ft For a ressure of 4 sia the saturation temerature T sat = 15.9 o F. mvaor 7 kg x = = = 0.41 m 10 kg + 7 kg total. Quality is determined on a mass basis so we have to use Table C-1E to get the secific volume of each hase in order to calculate the mass of each hase: 1

5 m V liquid 1 ft = = = 60.1 lbm v ft /lbm liquid f m V vaor 5 ft = = = 0.15 lbm v.6 ft /lbm vaor g mvaor 0.15 lbm x = = = = 0.5% m 60.1 lbm lbm total.4 At state 1 the water is a saturated liquid (x = 0). The secific volume v f at 00 kpa (0. MPa) can be found in Table C-: v f = m /kg. Then V 1 = mv f = 4 kg ( m /kg) = m At state the water is a saturated vaor at 00 kpa. The secific volume v g at 00 kpa (0. MPa) can be found in Table C-: v g = m /kg. Then V = mv g = 4 kg ( m /kg) =.54 m..5 At state 1 the water is a saturated liquid (x = 0). The secific volume v f at 400 kpa (0.4 MPa) can be found in Table C-: v f = m /kg. So V m m = = = 0.7 kg. (This mass stays constant for the rocess.) v m /kg f At state the water is a saturated vaor at 400 kpa. The secific volume v g at 400 kpa (0.4 MPa) can be found in Table C-: v g = m /kg. So V = mv g = 0.7 kg m /kg = m.6 We have a fixed mass of 10 kg and a quality x = 0.85 (V vaor = 8.5 kg) so the system is a saturated mixture. Table C- lists the secific volumes for saturated mixtures. a) For a ressure of 140 kpa: v = v f + x(v g v f ) v = ( ) = 1.05 m /kg V = 10 kg (1.05 m /kg) = 10.5 m V vaor = 8.5 kg (1.7 m /kg) = m and T = T sat = 109. C b) For a ressure of 00 kpa: v = v f + x(v g v f ) v = ( ) = 0.75 m /kg. V = 10 kg (0.75 m /kg) = 7.5 m V vaor = 8.5 kg ( m /kg) = 7.58 m and T = T sat = 10. C c) For a ressure of 000 kpa: v = v f + x(v g v f ) v = ( ) = m /kg. V = 10 kg ( m /kg) = m 1

6 V vaor = 8.5 kg ( m /kg) = m and T = T sat = 1.4 C.7 The water is 10 kg of a saturated mixture with a quality of 0.6 = m vaor /m total. The roerties can be obtained from Table C-1 for T = 40 C: v = v f + x(v g v f ) = ( ) = m /kg V = mv = 10 kg (11.71 m /kg) = m. V liquid = = m V vaor = 6 kg (19.5 m /kg) = m (The volume is essentially all vaor.) P = P sat = MPa = 7.8 kpa.8 Table C-E gives us English unit saturation information if we know the ressure. a) For P = 70 sia, T sat = 0.0 F b) For P = 150 sia, T sat = 58.5 F c) For P = 400 sia, T sat = F.9 P = atm 100 kpa/atm = 0.0 kpa or MPa which is below the lowest ressure in Table C-. The saturation temerature would be very near 0 C..0 To resond to this roblem, lease Google ressure cooker..1 We know that the water is a saturated mixture with a volume of 5 m and a quality of 70%. Table C-1 will give the roerties. a) For T = 10 C, P = P sat = MPa = kpa. V V 5 m = = = = kg v v + x ( v v ) ( ) f g f b) For T = 40 C, P = P sat =.44 MPa = 44 kpa. V V 5 m = = = = kg v v + x ( v v ) ( ) f g f c) For T = 70 C, P = P sat = 1.0 MPa. V V 5 m = = = = 115 kg v v + x ( v v ) ( ) f g f. Table C-1 lists the roerties for saturated water in SI units. For T = 50 C we get v f = m /kg and v g = 1.0 m /kg Initial volume: V 1 = 0.5 kg ( m /kg) = m Final volume: V = 0.5 kg (1.0 m /kg) = m A big change!. Since the container is rigid, the volume and secific volume stay constant. Table C-1 or C- gives the roerties at the critical oint: v = m /kg. a) Table C- gives roerties for saturated water. At MPa 14

7 v vf x = = = =.01% v v g f b) Table C- gives roerties for saturated water. At 1. MPa v vf x = = = = 1.4% v v g f c) Table C- gives roerties for saturated water. At 0.4 MPa v vf x = = = = 0.449% v v g f.4 The water is initially at 00 kpa and x = 0.1. We can calculate the constant secific volume of the rigid container using the information from Table C-: ( ) ( ) v= v + x v v = = m /kg f g f a) At 140 o C from Table C-1: P = 61. kpa v vf x = = = or 17.4% v v g f b) At 180 o C from Table C-1: P = 100 kpa v vf x = = = or 45.8% v v c) At 10 o C from Table C-1: P = 1906 kpa g f v vf x = = = or 85.6% v v g f.5 At state 1 the water is a subcooled liquid at 5⁰C, so an accurate estimate of the secific volume is to use vf at 5 C. From Table C-1, v 1 = m /kg. The secific volume at 10 C from Table C-1 is v f = m /kg. Hence, ΔV = m(v v 1) = 4 ( ) = m. Very little change..6 State 1: m = kg, T 1 = 0 C, and P 1 = 5 MPa. This is a subcooled liquid. State : m = kg, T = 00 C, and P = P 1 = 5 MPa. At this temerature the water remains a subcooled liquid since P < P sat = 1.55 MPa. i) Using Table C-4 for the secific volume at state 1, v 1 = m /kg. For state, v = m /kg. 15

8 ΔV = ( ) = m ii) Use Table C-1 to get the secific volumes using the v f values: v 1 = m /kg, v = m /kg ΔV = ( ) = m (essentially the same answer) Conclusion: Table C-1 can be used to find v for comressed liquids. Simly ignore the ressure..7 At state 1 the quality is zero and the ressure is 00 kpa or 0. MPa. Use Table C- to find v 1 = v f = m /kg. At state the ressure is MPa and the temerature is 400 C. Here the water is a suerheated vaor. Use Table C- to get the secific volume: v = m /kg. Then ΔV = ( ) = 0.00 m.8 At state 1 the water is a saturated mixture with a temerature of 10 C and a quality of 0.4. The ressure is the saturation ressure at 10 C which, from Table C-1, is MPa or 70.1 kpa. From this table we get the secific volumes for a saturated liquid v f and a saturated vaor v g to calculate v = v f + x(v g v f ) = ( ) = 0.68 m /kg V total = =.68 m The volume of liquid is V f = m /kg = m.9 The secific volume of the water is v = V/m = 70 ft /10 lbm = 7 ft /lbm. i) For v = 7 ft /lbm and P = 50 sia, use Table C-E to find that v f < 7 < v g. The water is a saturated mixture. ii) For v = 7 ft /lbm and P = 6 sia, use Table C-E to find that 7 > v g. The water is a suerheated vaor. At 61 sia, it would be a saturated mixture. iii) For v = 7 ft /lbm and P = 100 sia, use Table C-E to find that v > v g. The water is a suerheated vaor..40 The roblem states that the water is initially a saturated water vaor so x = 1. Knowing that T = 00 C we use table C-1 to get P 1 = P sat = 1554 kpa. The secific volume is v = v g = m /kg. a) If the temerature stays constant and the volume increases by 50%, v 1 = 1.5v = m /kg = m /kg which is in the suerheat range being greater than v g. We can use Table C- to get the roerties but this would require interolating between ressures of 1 MPa and 1. MPa. Use the IRC Calculator: P = 1070 kpa. b) If the temerature stays constant and we increase the volume by 100% v 1 = v 1 = m /kg = m /kg which is in the suerheat range being greater than ν g. We can use Table C- to get the roerties but this would require interolating between ressures of 0.8 MPa and 1 MPa. Use the IRC Calculator: P = 818 kpa. 16

9 c) If the temerature stays constant and we increase the volume by 00% v 1 = v = m /kg = 0.8 m /kg which is in the suerheat range being greater than ν g. We can use Table C- to get the roerties but this would require interolating between ressures of 0.4 MPa and 0.6 MPa. Use the IRC Calculator: P = 554 kpa..41 At 40 sia and 400 F the water is suerheated (P < P sat at 400 ). From Table C-E we get v = 1.6 ft /lbm: m = V/ v = 10 ft /1.6 ft /lbm = 0.79 lbm.4 a) For P = 5 MPa and T = 5 C the water is solid ice. Table C-5 gives the secific volume for ice to be m /kg: V = mv = 8 kg m /kg = m b) For P = 5 MPa and T = 0 C the water is a subcooled liquid. Table C-4 gives the secific volume for the water to be m /kg: V = mv = 8 kg m /kg = m c) For P = 5 MPa and T = 400 C the water is a suerheated vaor. Table C- gives the secific volume for the vaor to be m /kg: V = mv = 8 kg m /kg = m d) For P = 5 MPa and T = 800 C the water is a suerheated vaor. Table C- gives the secific volume for the vaor to be m /kg: V = mv = 8 kg m /kg = m.4 The weight of the iston is W = mg = 160 kg (9.81 m/s ) = N. The ressure caused by the weight of the iston: N P iston = W/A iston = π 0.1 m = Pa or 50 kpa The initial ressure is P 1 = P iston + P atm = 50 kpa kpa = 150 kpa. At the initial state, the ressure is 150 kpa and x = 1. The temerature is the saturation temerature at 150 kpa, which from Table C- is 111 o C, by interolation. Also by interolation, v 1 = v g = m /kg. Then V 1 = 0.0 kg m /kg = 0.0 m. a) To comress the sring 6 cm, the additional ressure is ( N/m)( 0.06 m) Kx P = A = π = N/m = 115 kpa 0.1 m So, P = 150 kpa kpa = 65 kpa. The volume is V = V + ΔV = 0.0 m m π(0.1 m) = 0.04 m The secific volume is then v = 0.04 m /0.0 kg = 1. m /kg. Using the IRC calculator with P = 65 kpa, the temerature is T = 418 C. 17

10 b) To comress the sring 10 cm, the additional ressure is ( N/m)( 0.1 m) Kx P = A = π = N/m = 191 kpa 0.1 m So, P = 150 kpa kpa = 41 kpa. The volume is V = V + ΔV = 0.0 m m π(0.1 m) = 0.05 m. The secific volume is then v = 0.05 m /0.0 kg = 1.5 m /kg. Using the IRC calculator with P = 41 kpa, the temerature is T = 65 C. c) To comress the sring 15 cm, the additional ressure is ( N/m)( 0.15 m) Kx P = A = π = N/m = 86 kpa 0.1 m So, P = 150 kpa + 86 kpa = 46 kpa. The volume is V = V + ΔV = 0.0 m m π(0.1 m) = 0.07 m The secific volume is then v = 0.07 m /0.0 kg = 1.5 m /kg. Using the IRC Calculator with P = 46 kpa, the temerature is T = 1010 C..44 The weight of the iston is W = mg = 160 kg 9.81 m/s = 1570 N. The ressure caused by the weight of the iston is W P = A = 1570 N π = N/m = 50 kpa 0.1 m The initial ressure P 1 = P iston + P atm = 50 kpa kpa = 150 kpa. For a ressure of 150 kpa and x = 0.8, we can calculate the secific volume using the data in Table C- between 0.14 MPa and 0.16 MPa. By interolation: v 1 = ( ) = 0.91 m /kg Also by interolation the saturation temerature is 111 o C. For the final state, the temerature is 800 o C which means the final state is robably a suerheated vaor. The only thing that stays constant in this roblem is the mass. We have to balance the osition of the iston, the ressure, and the temerature to find the final state. This must be done by trial and error. The initial volume in the cylinder can be calculated from state 1: For the final state T = 800 o C and P = 150 kpa + V 1 = 0.91 m /kg 0.0 kg = m ( 60 kn / m)x π 0.1 m, V m + ( π 0.1 x) m v = = m 0.0 kg 18

11 We must choose a value of the iston dislacement x so that all three roerties match in the steam tables. This occurs for x = 15 cm and P = 44 kpa. The quickest and easiest way to solve this is to use the IRC Calculator..45 From Problem.4, P initial = 150 kpa, x = 1, T 1 = 111. C, v 1 = m /kg and V 1 = 0.0 m. The iston must rise cm to reach the iston. This will be at constant ressure: P = 150 kpa, V = 0.0 m + [0.0 π (0.1) ] m = 0.06 m 0.06 m v = = 0.0 kg 1.1 m /kg Using the IRC Calculator with P = 150 kpa and v = 1.1 m /kg we get T = 111 o C and x = 0.975, a saturated mixture. At the final state, the sring is comressed 6 cm. Then V m = 0.06 m π 0.1 = m, v = = 1.5 m /kg 0.0 kg P = 150 kpa kpa = 65 kpa (from Problem.4) For P = 65 kpa and v = 1.5 m /kg we use the IRC Calculator to get T = 4 C, a suerheated vaor..46 Draw the diagrams to scale. Not many oints are needed to observe the general shae. Each diagram will resemble this sketch:.47 Use Table C-E to find the roerties for this saturated mixture at 50 sia by interolation between 00 sia and 00 sia:.48 The steam is at 1.86 MPa and 40 C. T = T sat = ( )/ = 400 F u f = ( )/ = 74 Btu/lbm u g = ( )/ = Btu/lbm h f = ( )/ = 74.9 Btu/lbm h g = ( )/ = Btu/lbm u = ( ) = 671 Btu/lbm h = ( ) = Btu/lbm i) Using Table C- we must double interolate for both ressure and temerature. P = 1.8 MPa P = MPa T = 400 C h = 50.9 h = 47.6 T = 500 C h = h = h 1.86MPa, 40 C = 94 kj/kg ii) For P = 1860 kpa and T = 40 C, use the IRC calculator: h = 90 kj/kg, u = 980 kj/kg, and v = m /k 19

12 iii) Using values from Part (ii) h = = 90 kj/kg (The numbers are to significant digits, so the answer is exressed with significant digits. All the answers are accetable. The fourth digit in Part (i) undoubtedly is meaningless. Significant digits are always lost when using straight-line interolations..49 At state 1 the water is saturated vaor (x = 1) at 00 F. At state the water is saturated liquid (x = 0). a) Use Table C-1E for the roerties. The saturation ressure at 00 F is sia and: v f = ft /lbm, u f = 69.5 Btu/lbm, h f = 69.7 Btu/lbm v g = 6.47 ft /lbm, u g = 1100 Btu/lbm, h g = Btu/lbm ΔV = 10 ( ) = ft ΔU = 10 ( ) = 805 Btu ΔH = 10 ( ) = 9105 Btu ΔH = ΔU + PΔV = (66.98 lbf/in )(144 in /ft ) (64.55 ft ) /778 ft-lbf/btu) = 9105 Btu b) Use the IRC Calculator for the roerties: P sat = 67 sia and: v f = ft /lbm, u f = 70 Btu/lbm, h f = 70 Btu/lbm v g = 6.47 ft /lbm, u g = 1100 Btu/lbm, h g = 1180 Btu/lbm ΔV = 10 ( ) = 64.5 ft ΔU = 10 ( ) = 800 Btu ΔH = 10 ( ) = 9100 Btu ΔH = ΔU + PΔV = (67 lbf/in )(144 in /ft ) (64.5 ft ) (1 Btu/778 ft-lbf) = 9100 Btu.50 State 1 is a saturated vaor (x = 1) at 00 o C. State is a suerheated vaor at MPa and 600 o C. a) The roerties for state 1 come from Table C-1: v 1 = v g = m /kg, h 1 = h g = 79. kj/kg The roerties for state come from Table C-: v = m /kg, h = kj/kg Δv = = 0.07 m /kg Δh = = kj/kg b) Use the IRC Calculator: v 1 = 0.17 m /kg, h 1 = 790 kj/kg v = 0. m /kg, h = 690 kj/kg Δv = = 0.07 m /kg Δh = = 900 kj/kg 0

13 .51 The ressure stays constant at 00 kpa: State 1: T 1 = 0 C, P 1 = 00 kpa (treat this as a saturated liquid at 0 C) State : T = 400 C, P = P 1 = 00 kpa or 0. MPa (suerheated vaor) a) The roerties for state 1 are from Table C-1 at 0 C: v 1 = v f = m /kg, u 1 = u f = 8.9 kj/kg, h 1 = h f = 8.9 kj/kg The roerties for state are from Table C- at 400 C: v = m /kg, u = kj/kg, Δρ = = 997 kg/m ΔU = 4 ( ) = kj ΔH = 4 ( ) = kj h = 76.6 kj/kg b) Use the IRC Calculator: At 0 C: v 1 = v f = m /kg, u 1 = u f = 8.9 kj/kg, h 1 = h f = 84.1 kj/kg At 400 C: v = 1.55 m /kg, u = 970 kj/kg, h = 80 kj/kg Δρ = = 999 kg/m ΔU = 4 ( ) = kj (the Calculator uses only significant digits) ΔH = 4 ( ) = kj.5 State 1: m = 0 kg, T 1 = 00 C, P 1 = 0.6 MPa suerheated State : T = 400 C, P = P 1 = 0.6 MPa suerheated a) Use Table C- for the enthalies: h 1 = kj/kg, h = 70. kj/kg. ΔH = 0 ( ) = 4174 kj b) Use the IRC Calculator for the enthalies: h 1 = 060 kj/kg, h = 70 kj/kg. ΔH = 0 (70 060) = 400 kj.5 You must determine the secific roerties in this roblem since you do not know the mass of the system. State 1: T 1 = 100 F, P 1 = 500 sia subcooled liquid State : T = 500 F P = P 1 = 500 sia suerheated vaor a) Use Table C-4E for the roerties at state 1: u 1 = Btu/lbm, h 1 = 69.6 Btu/lbm Use Table C-E for the roerties at state : u = Btu/lbm h = 11.5 Btu/lbm Δu = = 107 Btu/lbm Δh = = 116 Btu/lbm b) Use the IRC Calculator: 1

14 u 1 = 67.9 Btu/lbm, h 1 = 69.4 Btu/lbm, u = 1140 Btu/lbm, h = 10 Btu/lbm Δu = = 1070 Btu/lbm, Δh = = 1160 Btu/lbm.54 At state 1 the water is solid ice at 100 kpa and 0 C. The secific internal energy can be obtained from Table C-5: u 1 = 74 kj/kg At state the water is a subcooled liquid at 100 kpa and 0 C. The secific internal energy can be obtained from Table C-1 for T = 0 C: u = u f = 8.9 kj/kg ΔU = m(u g u i ) = 10 [8.9 ( 74)] = 4580 kj.55 The water is undergoing sublimation from solid ice at 0 C to a saturated vaor at 0 C. Table C-5 gives the roerties for these states:.56 We are given V = 0.05 m and m = 50 kg so ΔU = m(u g u i ) = 4 [48 ( 74)] = kj 0.05 m v = = m /kg 50 kg a) For P =.5 MPa or 500 kpa, from Table D-, we find the secific volume for a saturated liquid and a saturated vaor. v f = m /kg, v g = m /kg Since v is less than v f, the R14a is a subcooled liquid. b) For P = 40 kpa we use Table D- to obtain the saturation secific volumes. v f = m /kg, v g = m /kg Again, since v is greater than v f but less than v g, the R14a is a saturated mixture with x = = or 0.88% The secific volume of the refrigerant is 10 ft v = = 100 lbm 0.1 ft /lbm Use Table D-1E for T = 0 F: v f = ft /lbm, v g =.417 ft /lbm Since v f < v < v g the R14a is a saturated mixture with x = = or.60%

15 .58 At 00 kpa the saturation temerature of R14a is 1 C so the refrigerant is a subcooled liquid. Using Table D-1, the saturated liquid roerties at 1 C are v 1 = v f = m /kg, u 1 = u f = 4.5 kj/kg, h 1 = h f = 4.9 kj/kg At state the ressure remains constant at 00 kpa and T = 60 C. The refrigerant is now a suerheated vaor and we use Table D-: v = 0.1 m /kg, u = 78.1 kj/kg, h = 04.5 kj/kg. i) ΔV = 100 kg ( ) = 1.1 m ii) ΔU = 100 kg ( ) = 4 80 kj iii) ΔH = 100 kg ( ) = kj.59 State 1: T 1 = 80 F and x 1 = 0. See Table D-1E: P 1 = P sat = sia, h 1 = h f = 7.7 Btu/lbm State : P = 10 sia and h = h 1 = 7.7 Btu/lbm. We can get the enthaly data from Table D-E at 10 sia: h f =.91 Btu/lbm, h g = 97.7 Btu/lbm. Since h is between these two values, the state is a saturated mixture. The temerature at state is the saturation temerature of 9.7 F (very cold) and h= h + xh. 7.7 =.91 + x(94.45). x= 0.64 or 6.4% f fg.60 The working fluid is ammonia. State 1: T 1 = 40 C and x = From Table E-1: h f = 0.0 kj/kg, h fg = 189 kj/kg h 1 = = 10 kj/kg State : P = 400 kpa, T = 40 C. Use Table E- for suerheat: h = kj/kg. Δh = = 5 kj/kg.61 We know the mass, the ressure and the temerature of the air. Use the ideal gas law to determine the secific volume. Use Table B- to get the gas constant for air: v 1 kj K RT1 kg K = = = 0.7 m /kg. V 1 = mv 1 = = 0.07 m P 10 kpa 1 At the final state T = 5 C or 08 K kj K RT kg K v = = = 0.77 m /kg. V = mv = = m P 10 kpa In the above, the units convert as kj K kn m K m = =. kg K kpa kg K kn/m kg

16 .6 V = 4/ πr = (4/) π (1) = 4.19 ft, T = 7 F = 5 R, P = 14.7 sia ft lbf 5. 5 R RT lbm- R ft v = = = 1.40, P 14.7 lbf/in 144 in /ft lbm V m = = 4.19 ft = 0.1 lbm v 1.40 ft / lbm At 5000 ft the ressure is 0.8P 0 = sia) = 1. sia from Table B-1E. We assume that the temerature does not change: v RT 5. 5 R = = = 16.1 ft /lbm, V = mv= = 5.05 ft P Since V = πr = 5.05 ft, r = 1.06 ft and d=.1 ft..6 For carbon dioxide, Table B- gives R = kj/kg K. For P = 1 kpa and T = 60 C CO or 1 K. Then RT K v = = = 40.4 m /kg (See Problem.61 for units) P 1.64 The container has a constant volume of 5 m and an initial temerature of 00 K. Use the ideal gas law to find the final mass. The final ressure is 500 kpa: m PV = = = 9.04 kg (See Problem.61 for units.) RT Δm = = 8.8 kg.65 Initially, m = 10 lbm, P 1 = 14.7 sia, and T 1 = 80 F or 540 R: ft-lbf 10 lbm R mrt V = = lbm- R = 16 ft 1 1 P1 ( ) lbf/ft The final volume V = V 1 /4 = 16/4 = 4 ft. With P = 40 sia, lbf (40 144) 4 ft PV = = ft o T = 67 R mr ft lbf 10 lbm 5. lbm R.66 The gas is unknown so the gas constant is unknown. 4 v= = m /kg, From Table B- we see that the gas is helium. Pv 400 R = = =.077 kj/kg K T 85 4

17 .67 Convert the temerature to 9 K: 6 PV 100 ( 10 ) 6 m = = =.8 10 kg RT ( ) 6 7 W = mg=.8 10 kg 9.81 m/s =. 10 N or. MN.68 Given: V = 10 m i) ii) RT v = = = m /kg, ρ = = = 1.47 kg / m P 00 v W = mg = ρvg = = 145 N RT P = = = 410 kpa, ρ = = = 1.5 kg / m v 0.08 v 0.08 W = mg = ρvg = = 10 N,, iii) 40 = mg = ρvg = ρ ρ = kg/m, 1 1 v = = = ρ m /kg, Pv T = = = 510 K,or 4850 C R 0.87 iv) 1 1 RT 0.87 v= = = 0.05 m /kg, P = = = 17 kpa, ρ 0 v 0.05 W = mg = ρvg = = 1960 N,.69 Given: V = 0 ft i) ii) RT v = = = 15.9 ft /lbm, ρ = = = lbm/ft P v 15.9 W = mg = ρvg = = 60.7 lbf RT P 144 = = = 67 sia, ρ = = = 0.8 lbm/ft v 1. v 1. W = mg = ρvg = = 805 lbf,, iii) W = mg= ρvg= ρ 0. = 80. ρ = lbm/ft, 1 1 Pv ( ) 1.07 v= = = 1.07 ft /lbm, T = = = 61 R, or 800 F ρ R 5. iv) 1 1 P 144 = ρrt = = 7 sia, v= = = 0.65 lbm/ft ρ 1.6 W = mg = ρvg = = 1546 lbf, 5

18 .70 Inside the house T = 7 F or 5 R. If we assume that the ressure is 14.7 sia, ρ inside P = = = lbm/ft RT 5. 5 Outside the house T = 0 F or 440 R. We again assume that the ressure is atmosheric. ρ outside P = = = lbm/ft RT Δ ρ = = lbm/ft The change in density will cause the chimney effect: lighter articles rise and heavier articles fall. Hence, there exists a migration of air articles from the high density region to the low density region, i.e., from the inside to the outside near the to of the house. The heavier articles then enter near the bottom of the walls to take the lace of the vacating articles..71 P RT v T 1 60 = = = = 1.8 P v RT T with v = v. Then, the ressure in Arizona is 1 P = P 1.8 = ( ) 1.8 = 68.6 sia or 5.9 si gage 1 Don t multily 5 si by 1.8. You must use absolute ressures..7 Since the drag force is directly roortional to the density of the air, the higher the density the greater the drag force, which will cause the ball to not travel as far. The question is: Is humid air more dense or less dense than dry air? Consider the ideal gas law ρ = PRT / : P P P P ρ = = and ρ = =. ρ = 1.61ρ R T 0.87T R T 0.46T air humid dry air humid dry air steam The density of the dry air is greater than the density of humid air so the drag is greater on a dry day, contrary to what all those crazy golfers think! It is more uncomfortable on a humid day but we re talking about distance! If it weren t for the ideal gas law, the ball would travel further on that dry day. Was it the liberals or the conservatives who made u that law?.7 Find the gas constant R for nitrogen in Table B-: i) Using the ideal gas law, RT v = = = m/kg P 4000 ii) From Fig.. for P = 4 MPa and T = 10 K, we get Z = 0.4. Then ZRT v = = = m/kg P 4000 The ideal gas law does not give accetable results at high ressures and low temeratures. That combination is uncommon in our introductory course so it is not encountered very often. 6

19 .74 Given: m = 10 kg, V = 1 m, and T = 40 C or K. 1 v = = m/kg. a) i) Use Table B- for the gas constant of air. The ressure, using the ideal gas law, is RT 0.87 P = = = 669 kpa v 0.1 ii) The critical temerature and ressure for air are found in Table B-: 1 K,.77 MPa. The coefficients for van der Waals equation (.17) are found in Table B-10: RT a P = = = 661 kpa v b v b) Table. in Section.5 gives the coefficients of the Beattie-Bridgeman equation (.19) for air. A 0 = 11.84, B 0 = , a = , b = , c = The molar secific volume for air is m kg v = vm = =.90 m /kmol kg kmol RT c b A a = v vt v 1 v v = u 0 P v B 0 = 66 kpa c) Use the estimate of the ressure from Part (i) to find P R : P R = P T T 175 R P = 669 = 0.177, = T = = cr From Aendix Fig. H-1 for T R = 1.75 and P R = 0.177, the comressibility factor is about This rovides a ressure of P = = 66 kpa. d) The IRC calculator for dry air at 40 C and a density of 10 kg/m rovides P = 664 kpa..75 The working fluid is nitrogen at 80 F or 80 R with a secific volume of 0.6 ft /lbm. i) The ideal gas law is used to find RT P = = = 4,900 lbf/ft or 4 sia v 0.6 ii) Find the van der Waals coefficients in Table B-10. Equation (.17) rovides cr 7

20 RT a P = = =, 670 sfa or 4 sia v b v iii) Use the estimate of the ressure from Part (i) to find P R :.76 For air at 60 kpa and 80 C or 19K. P R = P T T 1 R P = 4 = 0.49, = T = 80 = cr From Fig. H-1, Z 0.96 so P = = sia. i) The ideal gas law is used to give RT v = = = 0.9 m/kg P 60 ii) The critical constants for air from Table B-are T cr = 1 K and P cr =.77 MPa. Use Table B-10 for the van der Waals coefficients and Eq..17 for v: RT a P = or 60 = v b v v v This equation is solved for v by trial and error. Use the value from Part (i) as a start: cr For v = 0.9, 60 =? For v = 0.9, 60 =? v = 0.91 m /kg. P T iii) P = T 1 R R P = 60 = 0.016, = T = 19 = cr Using Table H- we get Z v = 0.9 m /kg cr iv) The IRC Calculator for dry air at 80 C and a ressure of 60 kpa gives v = 0.9 m /kg..77 The secific heats are listed in Table B-. a) For air C P = 1.00 kj/kg C, Δh = 1.00 (450 C 0 C) = 40 kj/kg b) For nitrogen C P = 1.04 kj/kg C, Δh = 1.04 (450 0) = 448 kj/kg c) For hydrogen C P = kj/kg C, Δh = (450 0) = 6110 kj/kg d) For roane C P = kj/kg C, Δh = (450 0) = 7 kj/kg e) For steam C P = 1.87 kj/kg C, Δh = 1.87 (450 0) = 805 kj/kg.78 State 1: T 1 = 0 C and x 1 = 1 (Steam is very near an ideal gas at this state: check v = RT/ P.) State : T = 150 C and P = 00 kpa i) For steam, we use Table B- to get C P = 1.87 kj/kg C Δh = C P ΔT = 1.87(150 0) = 5 kj/kg g 8

21 ii) From Table C-1, h 1 = h g = 556. kj/kg. From Table C-, h = kj/kg Δh = = 1 kj/kg iii) Using the IRC calculator, we obtain h 1 = 560 kj/kg and h = 770 kj/kg Δh = = 10 kj/kg.79 a) i) Table B- gives the constant secific heats for nitrogen: Δu = kj/kg C(500 0 ) = 57.6 kj/kg Δh = 1.04 kj/kg C(500 0 ) = 479 kj/kg ii) Use Table F- for the molar internal energies and enthalies: kj / kmol 6190 kj / kmol Δ u = = 71 kj/kg 8 kg / kmol 085 kj / kmol 8669 kj / kmol Δ h = = 514 kj/kg 8 kg / kmol b) The average temerature is T av = ( )/ = 60 C or 5K 5 9 C = C = 9.9 kj/kmol K 9. 9 kj / kmol K = = kj/kg K 8 kg / kmol C = C R= = kj/kg K v Δ u = ( 500 0) = 70 kj/kg, Δ h = ( 500 0) = 51 kj/kg c) = = kj/kg K C C = C R= = kj / kg K v P Δ u= ( 500 0) = 70 kj/kg, Δ h= ( 50 ) = 51 kj/kg.80 m = 0 lbm of air and ΔT = 975 R a) i) From Table B- for air Cv = Btu/lbm- R and C = 0.4 Btu/lbm- R: Δ U = mc Δ T = = 0 Btu v Δ H = mc Δ T = = 4680 Btu ii) From Aendix F-1E: for air at 485 o R we get u 1 = 8.6 Btu/lbm and h 1 = Btu/lbm by interolation. For air at 1460 o R, u = 58.6 Btu/lbm and h = 58.6 Btu/lbm. ΔU = 0 ( ) = 50 Btu 9

22 ΔH = 0 ( ) = 4854 Btu b) Table B-6 is in SI units only. The roblem will have to be converted to SI, solved in SI and then converted back to English units. T 1 = 485 R or 69 K, T = 1460 R or 811 K, T av = 540 K For air: Table B-6 rovides Cv = kj/kg K and C = 1.04 kj/kg K (it is not necessary to be exact in the relatively easy interolation), so Δ U = mc Δ T = ( ) (811 69) = 69 kj or 500 Btu v Δ H = mc Δ T = ( ) 1.04 (811 69) = 5114 kj or 4850 Btu c) Again, we solve the roblem in SI units: C = T T T At the average temerature of 540 K, C = kj/kgk. Then C = C R= = kj/kg K v Δ U = mc Δ T = ( ) (811 69) = 80 kj or 60 Btu v Δ H = mc Δ T = ( ) (811 69) = 54 kj or 4670 Btu d) The IRC Calculator rovides the internal energies and enthalies for dry air at both temeratures. Using English units, ΔU = 0 (59 8.6) = 50 Btu ΔH = 0 (59 116) = 4860 Btu.81 For steam at 1600 kpa and 400 C, we use Table C- for the following enthalies: T ( C) h (kj/kg) i) Using backward differencing at 50 C and 400 C, there results C Δh = = =.18 kj/kg C Δ T 50 C ii) Use forward differencing at 50 C and 400 C: C Δh = = =.18 kj/kg C ΔT 100 iii) Use central differencing at 00 C and 500 C (the intervals must be the same): C Δh = = =.18 kj/kg C ΔT 150 0

23 iv) For steam at 00 K from Table B-, C = 1.87 kj/kg C The curve C (T) does not have sufficient curvature for a difference to aear in the three difference methods; however, central differencing should give the most accurate value of C at 400 C..8 Use the enthaly data for steam from Table C-. a) P = 0. MPa and T = 400 C. We will use central differencing between 00 and 500 to estimate the secific heat at 400 : C Δh = = =.08 kj/kg C ΔT 00 b) P = 1.8 MPa and T = 400 C. We will use central differencing between 00 and 500 to estimate the secific heat at 400 : C Δh = = =.0 kj/kg C ΔT 00 c) P = 7 MPa and T = 400 C. We will use central differencing between 50 and 450 to estimate the secific heat at 400 : C Δh = = =.71 kj/kg C ΔT Using enthaly data for steam from Table C-E. a) P = 40 sia and T = 600 F. We will use central differencing between 500 F and 700 F to get the secific heat at 600 F. C Δh = = = Btu/lbm- F ΔT 00 b) P = 140 sia and T = 600 F. We will use central differencing between 500 F and 700 F to get the secific heat at 600 F. C Δh = = = Btu/lbm- F ΔT 00 c) P = 600 sia and T = 600 F. We will use central differencing between 500 F and 700 F to get the secific heat at 600 F. C Δh = = = 0.67 Btu/lbm- F Δ T lbm of water is heated at 14.7 sia from 60 to 00. The water will exist as a subcooled liquid. The comressed liquid roerties will be aroximated by the saturated liquid roerties. Use Table C.1E to get the internal energies and enthalies: At 60 F, u 1 = u f = 8.08 Btu/lbm and h 1 = h f = 8.08 Btu/lbm. At 00 F, u = u f = Btu/lbm and h = h f = Btu/lbm 1

24 ΔU = 100 ( ) = 14,000 Btu ΔH = 100 ( ) = 14,000 Btu The actual difference is Δh Δ u=δ ( Pv) = PΔ v = ( ) ( ) = 1.7 ft-lbf/lbm or Btu/lbm.85 From Table B-4 we get for mercury at 10 C and 1 atm a value of C = 0.18 kj/kg C. ΔH = mc ΔT = ΔT = 00 kj ΔT = 90 C T final = 5 C + 90 C = 15 C. (Mercury boils at 57 C.).86 In this roblem, 10 kg of ice at 0 C is heated to become liquid water at 50 C. The hase change occurs at 0 C since the ressure is resumably atmosheric. a) If C =.1 kj/kg C, the enthaly change of the ice is ΔH ice = mc ΔT = 10.1 [0 ( 0)] = 40 kj As stated on Section..4, the heat of fusion for ice is 0 kj/kg, so that ΔH melt = 10 kg 0 kj/kg = 00 kj To heat the liquid water from 0 C to 50 C, use C from Table B-4: ΔH liquid = mc ΔT = = 090 kj ΔH total = 40 kj + 00 kj kj = 5810 kj b) Use the equation C, ice = T: Δ H = m C dt ice = 10 ( T) dt = 10.1(0 + 0) = 44 kj 0 As stated on Section..4, the heat of fusion for ice is 0 kj/kg, so that ΔH melt = 10 kg 0 kj/kg = 00 kj To heat the liquid water from 0 C to 50 C, use C from Table B-4: ΔH liquid = mc ΔT = = 090 kj ΔH total = 44 kj + 00 kj kj = 580 kj

Thermodynamic Properties are Measurements p,t,v, u,h,s - measure directly -measure by change

Thermodynamic Properties are Measurements p,t,v, u,h,s - measure directly -measure by change Thermodynamic Proerties are Measurements,T,, u,h,s - measure directly -measure by change s Tables T T Proerty Data Cure its Tables Correlation's, Boyles Law Tables c@tc limited hand calculations Equations

More information

THE FIRST LAW OF THERMODYNAMICS

THE FIRST LAW OF THERMODYNAMICS THE FIRST LA OF THERMODYNAMIS 9 9 (a) IDENTIFY and SET UP: The ressure is constant and the volume increases (b) = d Figure 9 Since is constant, = d = ( ) The -diagram is sketched in Figure 9 The roblem

More information

Chapter 4 Practice Problems

Chapter 4 Practice Problems Chater 4 ractice roblems (4.) (a) the number of microstates is N (b) 3 articles total 3! {, } 3 number microstates of secific arrangement (macrostate)!*! robability = (# microstates of secific arrangement)/(total

More information

To receive full credit all work must be clearly provided. Please use units in all answers.

To receive full credit all work must be clearly provided. Please use units in all answers. Exam is Open Textbook, Open Class Notes, Computers can be used (Computer limited to class notes, lectures, homework, book material, calculator, conversion utilities, etc. No searching for similar problems

More information

KNOWN: Data are provided for a closed system undergoing a process involving work, heat transfer, change in elevation, and change in velocity.

KNOWN: Data are provided for a closed system undergoing a process involving work, heat transfer, change in elevation, and change in velocity. Problem 44 A closed system of mass of 10 kg undergoes a process during which there is energy transfer by work from the system of 0147 kj per kg, an elevation decrease of 50 m, and an increase in velocity

More information

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium Pure Substance Properties of Pure Substances & Equations of State Dr. d. Zahurul Haq Professor Department of echanical Engineering Bangladesh University of Engineering & Technology (BUET) Dhaka-1000, Bangladesh

More information

I affirm that I have never given nor received aid on this examination. I understand that cheating in the exam will result in a grade F for the class.

I affirm that I have never given nor received aid on this examination. I understand that cheating in the exam will result in a grade F for the class. Chem340 Physical Chemistry for Biochemists Exam Mar 16, 011 Your Name _ I affirm that I have never given nor received aid on this examination. I understand that cheating in the exam will result in a grade

More information

GEF2200 vår 2017 Løsningsforslag sett 1

GEF2200 vår 2017 Løsningsforslag sett 1 GEF2200 vår 2017 Løsningsforslag sett 1 A.1.T R is the universal gas constant, with value 8.3143JK 1 mol 1. R is the gas constant for a secic gas, given by R R M (1) where M is the molecular weight of

More information

Chapter 4. Energy Analysis of Closed Systems

Chapter 4. Energy Analysis of Closed Systems Chapter 4 Energy Analysis of Closed Systems The first law of thermodynamics is an expression of the conservation of energy principle. Energy can cross the boundaries of a closed system in the form of heat

More information

Chemistry 531 Spring 2009 Problem Set 6 Solutions

Chemistry 531 Spring 2009 Problem Set 6 Solutions Chemistry 531 Sring 2009 Problem Set 6 Solutions 1. In a thermochemical study of N 2, the following heat caacity data were found: t 0 C,m d 27.2Jmol 1 K 1 f t b f C,m d 23.4Jmol 1 K 1 C,m d 11.4Jmol 1

More information

Thermodynamics I Chapter 2 Properties of Pure Substances

Thermodynamics I Chapter 2 Properties of Pure Substances Thermodynamics I Chapter 2 Properties of Pure Substances Mohsin Mohd Sies Fakulti Kejuruteraan Mekanikal, Universiti Teknologi Malaysia Properties of Pure Substances (Motivation) To quantify the changes

More information

PROBLEM 6.3. Using the appropriate table, determine the indicated property. In each case, locate the state on sketches of the T-v and T-s diagrams.

PROBLEM 6.3. Using the appropriate table, determine the indicated property. In each case, locate the state on sketches of the T-v and T-s diagrams. PROBLEM 63 Using the appropriate table, determine the indicated property In each case, locate the state on sketches of the -v and -s diagrams (a) water at p = 040 bar, h = 147714 kj/kg K Find s, in kj/kg

More information

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential Chem 467 Sulement to Lectures 33 Phase Equilibrium Chemical Potential Revisited We introduced the chemical otential as the conjugate variable to amount. Briefly reviewing, the total Gibbs energy of a system

More information

SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 4 SONNTAG BORGNAKKE VAN WYLEN. FUNDAMENTALS of. Thermodynamics. Sixth Edition

SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 4 SONNTAG BORGNAKKE VAN WYLEN. FUNDAMENTALS of. Thermodynamics. Sixth Edition SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 4 SONNTAG BORGNAKKE VAN WYLEN FUNDAMENTALS of Thermodynamics Sixth Edition CHAPTER 4 SUBSECTION PROB NO. Concept-Study Guide Problems 7- Simple processes 3-8

More information

Dr Ali Jawarneh. Hashemite University

Dr Ali Jawarneh. Hashemite University Dr Ali Jawarneh Department of Mechanical Engineering Hashemite University Examine the moving boundary work or P d work commonly encountered in reciprocating devices such as automotive engines and compressors.

More information

MAE 110A. Homework 3: Solutions 10/20/2017

MAE 110A. Homework 3: Solutions 10/20/2017 MAE 110A Homework 3: Solutions 10/20/2017 3.10: For H 2O, determine the specified property at the indicated state. Locate the state on a sketch of the T-v diagram. Given a) T 140 C, v 0.5 m 3 kg b) p 30MPa,

More information

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium Pure Substance Properties of Pure Substances & Equations of State Dr. d. Zahurul Haq Professor Department of echanical Engineering Bangladesh University of Engineering & Technology (BUET) Dhaka-1000, Bangladesh

More information

SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 3 SONNTAG BORGNAKKE VAN WYLEN. FUNDAMENTALS of. Thermodynamics. Sixth Edition

SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 3 SONNTAG BORGNAKKE VAN WYLEN. FUNDAMENTALS of. Thermodynamics. Sixth Edition SOLUTION MANUAL ENGLISH UNIT PROBLEMS CHAPTER 3 SONNTAG BORGNAKKE VAN WYLEN FUNDAMENTALS of Thermodynamics Sixth Edition CHAPTER 3 SUBSECTION PROB NO. Concept-Study Guide Problems 128-132 Phase diagrams

More information

CHAPTER 1 Basic Considerations

CHAPTER 1 Basic Considerations CHAPTER Basic Considerations FE-type Exam Review Problems: Problems. to. Chapter / Basic Considerations. (C) m = F/a or kg = N/m/s = N s /m. (B) [μ] = [τ/(/dy)] = (F/L )/(L/T)/L = F. T/L. (A) 8 9.6 0 Pa

More information

ME 201 Thermodynamics

ME 201 Thermodynamics ME 0 Thermodynamics Solutions First Law Practice Problems. Consider a balloon that has been blown up inside a building and has been allowed to come to equilibrium with the inside temperature of 5 C and

More information

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Chapter 3 PROPERTIES OF PURE SUBSTANCES Thermodynamics: An Engineering Approach Seventh Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2011 Chapter 3 PROPERTIES OF PURE SUBSTANCES Copyright The McGraw-Hill Companies, Inc. Permission

More information

Chapter 9 Practical cycles

Chapter 9 Practical cycles Prof.. undararajan Chater 9 Practical cycles 9. Introduction In Chaters 7 and 8, it was shown that a reversible engine based on the Carnot cycle (two reversible isothermal heat transfers and two reversible

More information

FUGACITY. It is simply a measure of molar Gibbs energy of a real gas.

FUGACITY. It is simply a measure of molar Gibbs energy of a real gas. FUGACITY It is simly a measure of molar Gibbs energy of a real gas. Modifying the simle equation for the chemical otential of an ideal gas by introducing the concet of a fugacity (f). The fugacity is an

More information

KNOWN: Pressure, temperature, and velocity of steam entering a 1.6-cm-diameter pipe.

KNOWN: Pressure, temperature, and velocity of steam entering a 1.6-cm-diameter pipe. 4.3 Steam enters a.6-cm-diameter pipe at 80 bar and 600 o C with a velocity of 50 m/s. Determine the mass flow rate, in kg/s. KNOWN: Pressure, temperature, and velocity of steam entering a.6-cm-diameter

More information

SPC 407 Sheet 6 - Solution Compressible Flow Fanno Flow

SPC 407 Sheet 6 - Solution Compressible Flow Fanno Flow SPC 407 Sheet 6 - Solution Comressible Flow Fanno Flow 1. What is the effect of friction on flow velocity in subsonic and suersonic Fanno flow? Friction increases the flow velocity in subsonic Fanno flow,

More information

The Second Law: The Machinery

The Second Law: The Machinery The Second Law: The Machinery Chater 5 of Atkins: The Second Law: The Concets Sections 3.7-3.9 8th Ed, 3.3 9th Ed; 3.4 10 Ed.; 3E 11th Ed. Combining First and Second Laws Proerties of the Internal Energy

More information

Liquid water static energy page 1/8

Liquid water static energy page 1/8 Liquid water static energy age 1/8 1) Thermodynamics It s a good idea to work with thermodynamic variables that are conserved under a known set of conditions, since they can act as assive tracers and rovide

More information

Download Solution Manual for Thermodynamics for Engineers 1st Edition by Kroos and Potter

Download Solution Manual for Thermodynamics for Engineers 1st Edition by Kroos and Potter Download Solution Manual for Thermodynamics for Engineers 1st Edition by Kroos and Potter Link download full: https://digitalcontentmarket.org/download/solutionmanual-for-thermodynamics-for-engineers-1st-edition-by-kroos-andpotter/

More information

Chapter 2: The Physical Properties of Pure Compounds

Chapter 2: The Physical Properties of Pure Compounds Chapter 2: The Physical Properties of Pure Compounds 2-10. The boiler is an important unit operation in the Rankine cycle. This problem further explores the phenomenon of boiling. A. When you are heating

More information

GAS. Outline. Experiments. Device for in-class thought experiments to prove 1 st law. First law of thermodynamics Closed systems (no mass flow)

GAS. Outline. Experiments. Device for in-class thought experiments to prove 1 st law. First law of thermodynamics Closed systems (no mass flow) Outline First law of thermodynamics Closed systems (no mass flow) Device for in-class thought experiments to prove 1 st law Rubber stops GAS Features: Quasi-equlibrium expansion/compression Constant volume

More information

Readings for this homework assignment and upcoming lectures

Readings for this homework assignment and upcoming lectures Homework #3 (group) Tuesday, February 13 by 4:00 pm 5290 exercises (individual) Thursday, February 15 by 4:00 pm extra credit (individual) Thursday, February 15 by 4:00 pm Readings for this homework assignment

More information

Phase transition. Asaf Pe er Background

Phase transition. Asaf Pe er Background Phase transition Asaf Pe er 1 November 18, 2013 1. Background A hase is a region of sace, throughout which all hysical roerties (density, magnetization, etc.) of a material (or thermodynamic system) are

More information

300 kpa 77 C. (d) If we neglect kinetic energy in the calculation of energy transport by mass

300 kpa 77 C. (d) If we neglect kinetic energy in the calculation of energy transport by mass 6-6- Air flows steadily a ie at a secified state. The diameter of the ie, the rate of flow energy, and the rate of energy transort by mass are to be determed. Also, the error oled the determation of energy

More information

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA SCIENCE FOR TECHNICIANS OUTCOME 3 - ENERGY TUTORIAL 2 HEAT

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA SCIENCE FOR TECHNICIANS OUTCOME 3 - ENERGY TUTORIAL 2 HEAT EDEXCEL NATIONAL CERTIFICATE/DIPLOMA SCIENCE FOR TECHNICIANS OUTCOME 3 - ENERGY TUTORIAL 2 HEAT 3. Energy Mechanical work, energy and power: work - energy relationship, gravitational potential energy,

More information

ME 201 Thermodynamics

ME 201 Thermodynamics Spring 01 ME 01 Thermodynamics Property Evaluation Practice Problems II Solutions 1. Air at 100 K and 1 MPa goes to MPa isenthapically. Determine the entropy change. Substance Type: Ideal Gas (air) Process:

More information

20 m neon m propane. g 20. Problems with solutions:

20 m neon m propane. g 20. Problems with solutions: Problems with solutions:. A -m tank is filled with a gas at room temperature 0 C and pressure 00 Kpa. How much mass is there if the gas is a) Air b) Neon, or c) Propane? Given: T7K; P00KPa; M air 9; M

More information

Chapter 20: Exercises: 3, 7, 11, 22, 28, 34 EOC: 40, 43, 46, 58

Chapter 20: Exercises: 3, 7, 11, 22, 28, 34 EOC: 40, 43, 46, 58 Chater 0: Exercises:, 7,,, 8, 4 EOC: 40, 4, 46, 8 E: A gasoline engine takes in.80 0 4 and delivers 800 of work er cycle. The heat is obtained by burning gasoline with a heat of combustion of 4.60 0 4.

More information

Ideal Gas Law. September 2, 2014

Ideal Gas Law. September 2, 2014 Ideal Gas Law Setember 2, 2014 Thermodynamics deals with internal transformations of the energy of a system and exchanges of energy between that system and its environment. A thermodynamic system refers

More information

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Chapter 3 PROPERTIES OF PURE SUBSTANCES Chapter 3 PROPERTIES OF PURE SUBSTANCES PURE SUBSTANCE Pure substance: A substance that has a fixed chemical composition throughout. Air is a mixture of several gases, but it is considered to be a pure

More information

Example problems. Chapter 3: The Kinetic Theory of Gases. Homework: 13, 18, 20, 23, 25, 27 (p )

Example problems. Chapter 3: The Kinetic Theory of Gases. Homework: 13, 18, 20, 23, 25, 27 (p ) Examle roblems Chater : he Kinetic heory o Gases Homework:, 8,,, 5, 7 (. 5-5) 9. An automobile tire has a volume o.64 x m and contains air at a gauge ressure (above atmosheric ressure) o 65 kpa when the

More information

First law of thermodynamics (Jan 12, 2016) page 1/7. Here are some comments on the material in Thompkins Chapter 1

First law of thermodynamics (Jan 12, 2016) page 1/7. Here are some comments on the material in Thompkins Chapter 1 First law of thermodynamics (Jan 12, 2016) age 1/7 Here are some comments on the material in Thomkins Chater 1 1) Conservation of energy Adrian Thomkins (eq. 1.9) writes the first law as: du = d q d w

More information

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics PHYS1001 PHYSICS 1 REGULAR Module Thermal Physics Chater 17 First Law of Thermodynamics References: 17.1 to 17.9 Examles: 17.1 to 17.7 Checklist Thermodynamic system collection of objects and fields. If

More information

CHAPTER. The First Law of Thermodynamics: Closed Systems

CHAPTER. The First Law of Thermodynamics: Closed Systems CHAPTER 3 The First Law of Thermodynamics: Closed Systems Closed system Energy can cross the boundary of a closed system in two forms: Heat and work FIGURE 3-1 Specifying the directions of heat and work.

More information

THERMODYNAMICS, FLUID AND PLANT PROCESSES. The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial.

THERMODYNAMICS, FLUID AND PLANT PROCESSES. The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial. THERMODYNAMICS, FLUID AND PLANT PROCESSES The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial. THERMODYNAMICS TUTORIAL 1 LIQUIDS VAPOURS - GASES SAE

More information

ME 201 Thermodynamics

ME 201 Thermodynamics Fall 204 ME 20 Thermodynamics Homework #8 Solutions. A rigid wall, insulated container is divided into two regions by a removable wall. One region contains 0. lb m of CO at 00 F, while the other region

More information

Dishwasher. Heater. Homework Solutions ME Thermodynamics I Spring HW-1 (25 points)

Dishwasher. Heater. Homework Solutions ME Thermodynamics I Spring HW-1 (25 points) HW-1 (25 points) (a) Given: 1 for writing given, find, EFD, etc., Schematic of a household piping system Find: Identify system and location on the system boundary where the system interacts with the environment

More information

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS HET, ORK, ND THE FIRST L OF THERMODYNMIS 8 EXERISES Section 8. The First Law of Thermodynamics 5. INTERPRET e identify the system as the water in the insulated container. The roblem involves calculating

More information

QUIZZES RIEPJCPIγPJEJJJY

QUIZZES RIEPJCPIγPJEJJJY Che 3021 Thermodynamics I QUIZZES RIEPJCPIγPJEJJJY QUIZ 1. Find Molecular Weights: 1 1 CO 2 2 NaCl 3 Aspirin C 9 H 8 O 4 CO2 = NaCl = C9H8O4 = PIgPJC Quiz 1. Temperature conversion 1 Convert 94 o F, to

More information

Name: Self Assessment - Preparatory

Name: Self Assessment - Preparatory Name: Self Assessment - Preparatory 1. I have read the chapter before coming to the discussion session today. 2. I am able to state that a system is simply a space or mass that I choose to study. 3. I

More information

Chapter 3 PROPERTIES OF PURE SUBSTANCES SUMMARY

Chapter 3 PROPERTIES OF PURE SUBSTANCES SUMMARY Chapter 3 PROPERTIES OF PURE SUBSTANCES SUMMARY PURE SUBSTANCE Pure substance: A substance that has a fixed chemical composition throughout. Compressed liquid (sub-cooled liquid): A substance that it is

More information

Basic Thermodynamics Module 1

Basic Thermodynamics Module 1 Basic Thermodynamics Module 1 Lecture 9: Thermodynamic Properties of Fluids Thermodynamic Properties of fluids Most useful properties: Properties like pressure, volume and temperature which can be measured

More information

1 atm = 1.01x10 Pa = 760 Torr = 14.7 lb / in

1 atm = 1.01x10 Pa = 760 Torr = 14.7 lb / in Last class we began discussion of ressure in fluids, with ressure defined as, F = ; units N 1 Pa = 1 m 2 There are a number of other ressure units in common use having the following equivalence, 5 2 1

More information

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Chapter 3 PROPERTIES OF PURE SUBSTANCES Thermodynamics: An Engineering Approach Seventh Edition in SI Units Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2011 Chapter 3 PROPERTIES OF PURE SUBSTANCES Copyright The McGraw-Hill Companies, Inc.

More information

ME 2322 Thermodynamics I PRE-LECTURE Lesson 10 Complete the items below Name:

ME 2322 Thermodynamics I PRE-LECTURE Lesson 10 Complete the items below Name: Lesson 10 1. (5 pt) If P > P sat (T), the phase is a subcooled liquid. 2. (5 pt) if P < P sat (T), the phase is superheated vapor. 3. (5 pt) if T > T sat (P), the phase is superheated vapor. 4. (5 pt)

More information

Chapter 1 Fundamentals

Chapter 1 Fundamentals Chater Fundamentals. Overview of Thermodynamics Industrial Revolution brought in large scale automation of many tedious tasks which were earlier being erformed through manual or animal labour. Inventors

More information

ME 201 Thermodynamics

ME 201 Thermodynamics 8 ME 0 Thermodynamics Practice Problems or Property Evaluation For each process described below provide the temperature, pressure, and speciic volume at each state and the change in enthalpy, internal

More information

CHAPTER 1 Basic Considerations

CHAPTER 1 Basic Considerations CHAPTER 1 Basic Considerations FE-type Exam Review Problems: Problems 1.1 to 1.1. 1.1 (C) m F/a or kg N/m/s N. s /m. 1. (B) [µ] [τ//dy] (F/L )/(L/T)/L F. T/L. Chapter 1 / Basic Considerations 1. (A) 8

More information

Chapter 3 PROPERTIES OF PURE SUBSTANCES. Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008

Chapter 3 PROPERTIES OF PURE SUBSTANCES. Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008 Chapter 3 PROPERTIES OF PURE SUBSTANCES Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008 Objectives Introduce the concept of a pure substance. Discuss

More information

Temperature and Heat. Two systems of temperature. Temperature conversions. PHY heat - J. Hedberg

Temperature and Heat. Two systems of temperature. Temperature conversions. PHY heat - J. Hedberg Temperature and Heat 1. Two systems of temperature 1. Temperature conversions 2. Real science (one scale to rule them all) 3. Temperature scales 2. Effects of temperature on materials 1. Linear Thermal

More information

EVALUATING PROPERTIES FOR A PURE SUBSTANCES. By Ertanto Vetra

EVALUATING PROPERTIES FOR A PURE SUBSTANCES. By Ertanto Vetra EVALUATING PROPERTIES FOR A PURE SUBSTANCES 1 By Ertanto Vetra Outlines - TV, PV, PT, PVT Diagram - Property Tables - Introduction to Enthalpy - Reference State & Reference Values - Ideal Gas Equation

More information

Thermodynamics I Spring 1432/1433H (2011/2012H) Saturday, Wednesday 8:00am - 10:00am & Monday 8:00am - 9:00am MEP 261 Class ZA

Thermodynamics I Spring 1432/1433H (2011/2012H) Saturday, Wednesday 8:00am - 10:00am & Monday 8:00am - 9:00am MEP 261 Class ZA Thermodynamics I Spring 1432/1433H (2011/2012H) Saturday, Wednesday 8:00am - 10:00am & Monday 8:00am - 9:00am MEP 261 Class ZA Dr. Walid A. Aissa Associate Professor, Mech. Engg. Dept. Faculty of Engineering

More information

CHAPTER 2 Fluid Statics

CHAPTER 2 Fluid Statics Chater / Fluid Statics CHAPTER Fluid Statics FE-tye Exam Review Problems: Problems - to -9. (C) h (.6 98) (8.5.54) 96 6 Pa Hg. (D) gh 84. 9.8 4 44 76 Pa. (C) h h. 98. 8 Pa w atm x x water w.4 (A) H (.6

More information

Mechanical Engineering Department Third year class Gas Dynamics Tables Lecturer: Dr.Naseer Al-Janabi

Mechanical Engineering Department Third year class Gas Dynamics Tables Lecturer: Dr.Naseer Al-Janabi Mechanical Engineering Department Third year class Gas Dynamics Tables Lecturer: Dr.Naseer Al-Janabi Ref. Fundamentals of Gas Dynamics, 2e - R. Zucker, O. Biblarz Appendixes A. B. C. D. E. F. G. H. I.

More information

PROPERTIES OF PURE SUBSTANCES. Chapter 3. Mehmet Kanoglu. Thermodynamics: An Engineering Approach, 6 th Edition. Yunus A. Cengel, Michael A.

PROPERTIES OF PURE SUBSTANCES. Chapter 3. Mehmet Kanoglu. Thermodynamics: An Engineering Approach, 6 th Edition. Yunus A. Cengel, Michael A. Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008 Chapter 3 PROPERTIES OF PURE SUBSTANCES Mehmet Kanoglu Copyright The McGraw-Hill Companies, Inc.

More information

CHAPTER 2 Fluid Statics

CHAPTER 2 Fluid Statics Chater / Fluid Statics CHAPTER Fluid Statics FE-tye Exam Review Problems: Problems - to -9. (C) h (.6 98) (8.5.54) 96 6 Pa Hg. (D) gh 84. 9.8 4 44 76 Pa. (C) h h. 98. 8 Pa w atm x x water w.4 (A) H (.6

More information

Eng Thermodynamics I conservation of mass; 2. conservation of energy (1st Law of Thermodynamics); and 3. the 2nd Law of Thermodynamics.

Eng Thermodynamics I conservation of mass; 2. conservation of energy (1st Law of Thermodynamics); and 3. the 2nd Law of Thermodynamics. Eng3901 - Thermodynamics I 1 1 Introduction 1.1 Thermodynamics Thermodynamics is the study of the relationships between heat transfer, work interactions, kinetic and potential energies, and the properties

More information

! =!"#$% exerted by a fluid (liquid or gas) !"#$ =!"# FUNDAMENTAL AND MEASURABLE INTENSIVE PROPERTIES PRESSURE, TEMPERATURE AND SPECIFIC VOLUME

! =!#$% exerted by a fluid (liquid or gas) !#$ =!# FUNDAMENTAL AND MEASURABLE INTENSIVE PROPERTIES PRESSURE, TEMPERATURE AND SPECIFIC VOLUME FUNDAMENTAL AND MEASURABLE INTENSIVE PROPERTIES PRESSURE, TEMPERATURE AND SPECIFIC VOLUME PRESSURE, P! =!"#$%!"#! exerted by a fluid (liquid or gas) Thermodynamic importance of pressure One of two independent

More information

Example problems. Chapter 2: Temperature, heat, and the 1 st law of Thermodynamic. Homework: 2, 3, 4, 5, 6, 10, 15, 19, 21 (pages )

Example problems. Chapter 2: Temperature, heat, and the 1 st law of Thermodynamic. Homework: 2, 3, 4, 5, 6, 10, 15, 19, 21 (pages ) Examle roblems Chater : emerature, heat, and the 1 st law of hermodynamic Homework:,, 4, 5, 6, 1, 15, 19, 1 (ages 5-51) . (Page 5) wo constant-volume gas thermometers are assembled, one with nitrogen and

More information

1.4 Perform the following unit conversions: (b) (c) s. g s. lb min. (d) (e) in. ft s. m 55 h. (f) ft s. km h. (g)

1.4 Perform the following unit conversions: (b) (c) s. g s. lb min. (d) (e) in. ft s. m 55 h. (f) ft s. km h. (g) 1.4 Perform the following unit conversions: 0.05 ft 1 in. (a) 1L 61in. 1L 1ft (b) 1kJ 650 J 10 J 1Btu 1.0551kJ 0.616 Btu (c) 41 Btu/h 0.15 kw 1kW 1h 600 s 778.17 ft lbf 1Btu ft lbf 99.596 s (d) g 78 s

More information

Thermodynamics I. Properties of Pure Substances

Thermodynamics I. Properties of Pure Substances Thermodynamics I Properties of Pure Substances Dr.-Eng. Zayed Al-Hamamre 1 Content Pure substance Phases of a pure substance Phase-change processes of pure substances o Compressed liquid, Saturated liquid,

More information

Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10

Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10 Problem 1.6 Make a guess at the order of magnitude of the mass (e.g., 0.01, 0.1, 1.0, 10, 100, or 1000 lbm or kg) of standard air that is in a room 10 ft by 10 ft by 8 ft, and then compute this mass in

More information

Unit code: H/ QCF level: 5 Credit value: 15 OUTCOME 1 - THERMODYNAMIC SYSTEMS TUTORIAL 2

Unit code: H/ QCF level: 5 Credit value: 15 OUTCOME 1 - THERMODYNAMIC SYSTEMS TUTORIAL 2 Unit 43: Plant and Process Princiles Unit code: H/60 44 QCF level: 5 Credit value: 5 OUCOME - HERMODYNAMIC SYSEMS UORIAL Understand thermodynamic systems as alied to lant engineering rocesses hermodynamic

More information

Chapter 1 Solutions Engineering and Chemical Thermodynamics 2e Wyatt Tenhaeff Milo Koretsky

Chapter 1 Solutions Engineering and Chemical Thermodynamics 2e Wyatt Tenhaeff Milo Koretsky Chapter 1 Solutions Engineering and Chemical Thermodynamics 2e Wyatt Tenhaeff Milo Koretsky School of Chemical, Biological, and Enironmental Engineering Oregon State Uniersity 1.1 (b) The olume of water

More information

TDEC202 - Energy II (Recitation #3)

TDEC202 - Energy II (Recitation #3) TDEC202 - Energy II (Recitation #3) Summer Term, 2007 M. Carchidi Solution to Problem 3-029 We are given that the substance is R-134a and metric units so that Tables A-11, A-12 and A-13 in Appendix 1 will

More information

Common Terms, Definitions and Conversion Factors

Common Terms, Definitions and Conversion Factors 1 Common Terms, Definitions and Conversion Factors 1. Force: A force is a push or pull upon an object resulting from the object s interaction with another object. It is defined as Where F = m a F = Force

More information

Index to Tables in SI Units

Index to Tables in SI Units Index to Tables in SI Units Table A-1 Atomic or Molecular Weights and Critical Properties of Selected Elements and Compounds 926 Table A-2 Properties of Saturated Water (Liquid Vapor): Temperature Table

More information

ES201 - Examination 2 Fall Instructor: NAME BOX NUMBER

ES201 - Examination 2 Fall Instructor: NAME BOX NUMBER ES201 - Examination 2 Fall 2003-2004 Instructor: Class Period NAME BOX NUMBER Problem 1 ( 22 ) Problem 2 ( 26 ) Problem 3 ( 26 ) Problem 4 ( 26 ) Total (100) INSTRUCTIONS Closed book/notes exam. (Unit

More information

Chapter 10 Temperature and Heat

Chapter 10 Temperature and Heat Chapter 10 Temperature and Heat Thermodynamics deals with 1. Temperature. 2. The transfer and transformation of energy. 3. The relationship between macroscopic properties and microscopic dynamics. Temperature

More information

Thermodynamics Basics Enthalpy, Entropy, Molliers Diagram and Steam Tables By

Thermodynamics Basics Enthalpy, Entropy, Molliers Diagram and Steam Tables By Thermodynamics Basics Enthalpy, Entropy, Molliers Diagram and Steam Tables By S. Bobby Rauf, P.E., CEM, MBA Credit: 8 PDH Thermodynamics Fundamentals Series 1 Preface As the adage goes, a picture is worth

More information

Introduction to Engineering thermodynamics 2 nd Edition, Sonntag and Borgnakke. Solution manual

Introduction to Engineering thermodynamics 2 nd Edition, Sonntag and Borgnakke. Solution manual Introduction to Engineering thermodynamics nd Edition, Sonntag and Borgnakke Solution manual Chapter 4 Claus Borgnakke The picture is a false color thermal image of the space shuttle s main engine. The

More information

Day 3. Fluid Statics. - pressure - forces

Day 3. Fluid Statics. - pressure - forces Day 3 Fluid Statics - ressure - forces we define fluid article: small body of fluid with finite mass but negligible dimension (note: continuum mechanics must aly, so not too small) we consider a fluid

More information

CHAPTER. Properties of Pure Substances

CHAPTER. Properties of Pure Substances CHAPTER 2 Properties of Pure Substances A Pure Substance Is a substance that is chemically homogenous and fixed in chemical composition.(e.g. water, nitrogen, air & etc.) mixture of oil and water is not

More information

Phase Changes and Latent Heat

Phase Changes and Latent Heat Review Questions Why can a person remove a piece of dry aluminum foil from a hot oven with bare fingers without getting burned, yet will be burned doing so if the foil is wet. Equal quantities of alcohol

More information

Chapter 19 Entropy Pearson Education, Inc. Slide 20-1

Chapter 19 Entropy Pearson Education, Inc. Slide 20-1 Chapter 19 Entropy Slide 20-1 Ch 19 & 20 material What to focus on? Just put out some practice problems for Ch. 19/20 Ideal gas how to find P/V/T changes. How to calculate energy required for a given T

More information

Course: TDEC202 (Energy II) dflwww.ece.drexel.edu/tdec

Course: TDEC202 (Energy II) dflwww.ece.drexel.edu/tdec Course: TDEC202 (Energy II) Thermodynamics: An Engineering Approach Course Director/Lecturer: Dr. Michael Carchidi Course Website URL dflwww.ece.drexel.edu/tdec 1 Course Textbook Cengel, Yunus A. and Michael

More information

Outline. Example. Solution. Property evaluation examples Specific heat Internal energy, enthalpy, and specific heats of solids and liquids Examples

Outline. Example. Solution. Property evaluation examples Specific heat Internal energy, enthalpy, and specific heats of solids and liquids Examples Outline Property ealuation examples Specific heat Internal energy, enthalpy, and specific heats of solids and liquids s A piston-cylinder deice initially contains 0.5m of saturated water apor at 00kPa.

More information

MAE 11. Homework 8: Solutions 11/30/2018

MAE 11. Homework 8: Solutions 11/30/2018 MAE 11 Homework 8: Solutions 11/30/2018 MAE 11 Fall 2018 HW #8 Due: Friday, November 30 (beginning of class at 12:00p) Requirements:: Include T s diagram for all cycles. Also include p v diagrams for Ch

More information

Chemical Engineering Thermodynamics Spring 2002

Chemical Engineering Thermodynamics Spring 2002 10.213 Chemical Engineering Thermodynamics Spring 2002 Test 2 Solution Problem 1 (35 points) High pressure steam (stream 1) at a rate of 1000 kg/h initially at 3.5 MPa and 350 ºC is expanded in a turbine

More information

Chapter 3 First Law of Thermodynamics and Energy Equation

Chapter 3 First Law of Thermodynamics and Energy Equation Fundamentals of Thermodynamics Chapter 3 First Law of Thermodynamics and Energy Equation Prof. Siyoung Jeong Thermodynamics I MEE0-0 Spring 04 Thermal Engineering Lab. 3. The energy equation Thermal Engineering

More information

The average velocity of water in the tube and the Reynolds number are Hot R-134a

The average velocity of water in the tube and the Reynolds number are Hot R-134a hater 0:, 8, 4, 47, 50, 5, 55, 7, 75, 77, 8 and 85. 0- Refrigerant-4a is cooled by water a double-ie heat exchanger. he overall heat transfer coefficient is to be determed. Assumtions he thermal resistance

More information

Calculators are permitted. Computers, PDAs, and other electronic devices with a keyboard are not. Cell phones may not be used as calculators.

Calculators are permitted. Computers, PDAs, and other electronic devices with a keyboard are not. Cell phones may not be used as calculators. Chem. 30 Sring 008 Exam 3 VERSION A Professors Williams/Whetten his test is closed note/book One 8.5 x handwritten crib sheet (one sided) is ermitted. Please turn off your cell hone. Use a # encil. Calculators

More information

Pure Substances Phase Change, Property Tables and Diagrams

Pure Substances Phase Change, Property Tables and Diagrams Pure Substances Phase Change, Property Tables and Diagrams In this chapter we consider the property values and relationships of a pure substance (such as water) which can exist in three phases - solid,

More information

Fundamentals of Thermodynamics SI Version

Fundamentals of Thermodynamics SI Version Solution Manual Chapter 2 Fundamentals of hermodynamics SI Version Borgnakke Sonntag 8e Updated July 2013 2 Borgnakke and Sonntag CONEN CHAPER 2 SUBSECION PROB NO. Concept problems 1-15 Phase diagrams,

More information

CHAPTER 8 ENTROPY. Blank

CHAPTER 8 ENTROPY. Blank CHAPER 8 ENROPY Blank SONNAG/BORGNAKKE SUDY PROBLEM 8-8. A heat engine efficiency from the inequality of Clausius Consider an actual heat engine with efficiency of η working between reservoirs at and L.

More information

First Name Last Name CIRCLE YOUR LECTURE BELOW: Div. 1 10:30 am Div. 2 2:30 pm Div. 3 4:30 pm Prof. Gore Prof. Udupa Prof. Chen

First Name Last Name CIRCLE YOUR LECTURE BELOW: Div. 1 10:30 am Div. 2 2:30 pm Div. 3 4:30 pm Prof. Gore Prof. Udupa Prof. Chen CIRCLE YOUR LECURE BELOW: Div. 1 10:30 am Div. :30 m Div. 3 4:30 m Prof. Gore Prof. Udua Prof. Chen EXAM # 3 INSRUCIONS 1. his is a closed book examination. All needed roerty tables are rovided.. Do not

More information

Chapter 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

Chapter 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES 5- Chapter 5 MASS AND ENERGY ANALYSIS OF CONTROL OLUMES Conseration of Mass 5-C Mass, energy, momentum, and electric charge are consered, and olume and entropy are not consered durg a process. 5-C Mass

More information

NAME: AME Thermodynamics Examination 1: SOLUTION Prof. J. M. Powers 12 February 2010

NAME: AME Thermodynamics Examination 1: SOLUTION Prof. J. M. Powers 12 February 2010 NAME: AME 0 Thermodynamics Examination : SOLUTION Prof. J. M. Powers February 00 The advantageous use of Steam-power is unquestionably a modern discovery. And yet as much as two thousand years ago the

More information

df da df = force on one side of da due to pressure

df da df = force on one side of da due to pressure I. Review of Fundamental Fluid Mechanics and Thermodynamics 1. 1 Some fundamental aerodynamic variables htt://en.wikiedia.org/wiki/hurricane_ivan_(2004) 1) Pressure: the normal force er unit area exerted

More information

0.5 kpa (1000 Pa/kPa) *A. A = 70*9.81 N/500 N/m 2 = 1.37 m 2

0.5 kpa (1000 Pa/kPa) *A. A = 70*9.81 N/500 N/m 2 = 1.37 m 2 AREN 2110 Spring 2010 Homework #2: Due Friday, Jan 29, 6 PM Solutions 1. Consider a 70-kg woman who has a total footprint area of 400 cm2. She wishes to walk on the snow, but the snow cannot withstand

More information