20 Pages

YF_ISM_19

Course: MAE 162D, Spring 2012
School: UCLA
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FIRST THE LAW OF THERMODYNAMICS 19 The pV-diagram is sketched in Figure 19.1 19.1. (a) IDENTIFY and SET UP: The pressure is constant and the volume increases. Figure 19.1 (b) W = V2 V1 p dV V2 V1 Since p is constant, W = p dV = p(V2 - V1 ) The problem gives T rather than p and V, so use the ideal gas law to rewrite the expression for W. EXECUTE: pV = nRT so p1V1 = nRT1 , p2V2 = nRT2 ; subtracting the two...

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FIRST THE LAW OF THERMODYNAMICS 19 The pV-diagram is sketched in Figure 19.1 19.1. (a) IDENTIFY and SET UP: The pressure is constant and the volume increases. Figure 19.1 (b) W = V2 V1 p dV V2 V1 Since p is constant, W = p dV = p(V2 - V1 ) The problem gives T rather than p and V, so use the ideal gas law to rewrite the expression for W. EXECUTE: pV = nRT so p1V1 = nRT1 , p2V2 = nRT2 ; subtracting the two equations gives p (V2 - V1 ) = nR (T2 - T1 ) Thus W = nR (T2 - T1 ) is an alternative expression for the work in a constant pressure process for an ideal gas. Then W = nR (T2 - T1 ) = (2.00 mol)(8.3145 J/mol K)(107C - 27C) = +1330 J EVALUATE: The gas expands when heated and does positive work. IDENTIFY: At constant pressure, W = pV = nRT . R = 8.3145 J/mol K. T has the same numerical value in kelvins and in C. W 1.75 103 J = = 35.1 K. TK = TC and T2 = 27.0C + 35.1C = 62.1C. EXECUTE: T = nR (6 mol) (8.3145 J/mol K) EVALUATE: When W > 0 the gas expands. When p is constant and V increases, T increases. IDENTIFY: Example 19.1 shows that for an isothermal process W = nRT ln( p1 / p2 ). pV = nRT says V decreases when p increases and T is constant. SET UP: T = 358.15 K. p2 = 3 p1. EXECUTE: (a) The pV-diagram is sketched in Figure 19.3. p (b) W = (2.00 mol)(8.314 J/mol K)(358.15 K)ln 1 = -6540 J. 3 p1 EVALUATE: Since V decreases, W is negative. SET UP: 19.2. 19.3. Figure 19.3 19.4. IDENTIFY: Use the expression for W that is appropriate to this type of process. SET UP: The volume is constant. EXECUTE: (a) The pV diagram is given in Figure 19.4. (b) Since V = 0, W = 0. 19-1 19-2 Chapter 19 EVALUATE: For any constant volume process the work done is zero. Figure 19.4 19.5. IDENTIFY: Example 19.1 shows that for an isothermal process W = nRT ln( p1 / p2 ). Solve for p1. SET UP: For a compression (V decreases) W is negative, so W = -518 J. T = 295.15 K. p p W W -518 J = ln 1 . 1 = eW / nRT . = = -0.692. nRT p2 p2 nRT (0.305 mol)(8.314 J/mol K)(295.15 K) p1 = p2eW / nRT = (1.76 atm)e -0.692 = 0.881 atm. (b) In the process the pressure increases and the volume decreases. The pV-diagram is sketched in Figure 19.5. EVALUATE: W is the work done by the gas, so when the surroundings do work on the gas, W is negative. EXECUTE: (a) Figure 19.5 19.6. (a) IDENTIFY and SET UP: The pV-diagram is sketched in Figure 19.6. Figure 19.6 (b) Calculate W for each process, using the expression for W that applies to the specific type of process. EXECUTE: 1 2, V = 0, so W = 0 23 p is constant; so W = p V = (5.00 105 Pa)(0.120 m3 - 0.200 m3 ) = -4.00 104 J (W is negative since the volume decreases in the process.) Wtot = W1 2 + W2 3 = -4.00 10 4 J EVALUATE: The volume decreases so the total work done is negative. IDENTIFY: Calculate W for each step using the appropriate expression for each type of process. SET UP: When p is constant, W = pV . When V = 0, W = 0. EXECUTE: (a) W13 = p1 (V2 - V1 ), W32 = 0, W24 = p2 (V1 - V2 ) and W41 = 0. The total work done by the system is 19.7. 19.8. W13 + W32 + W24 + W41 = ( p1 - p2 )(V2 - V1 ), which is the area in the pV plane enclosed by the loop. (b) For the process in reverse, the pressures are the same, but the volume changes are all the negatives of those found in part (a), so the total work is negative of the work found in part (a). EVALUATE: When V > 0, W > 0 and when V < 0, W < 0. IDENTIFY: Apply U = Q - W . SET UP: For an ideal gas, U depends only on T. The First Law of Thermodynamics 19-3 19.9. EXECUTE: (a) V decreases and W is negative. (b) Since T is constant, U = 0 and Q = W . Since W is negative, Q is negative. (c) Q = W , the magnitudes are the same. EVALUATE: Q < 0 means heat flows out of the gas. The plunger does positive work on the gas. The energy added by the positive work done on the gas leaves as heat flow out of the gas and the internal energy of the gas is constant. IDENTIFY: U = Q - W . For a constant pressure process, W = pV . SET UP: Q = +1.15 105 J, since heat enters the gas. EXECUTE: (a) W = pV = (1.80 105 Pa)(0.320 m3 - 0.110 m3 ) = 3.78 104 J. (b) U = Q - W = 1.15 105 J - 3.78 10 4 J = 7.72 10 4 J. EVALUATE: (c) W = pV for a constant pressure process and U = Q - W both apply to any material. The ideal gas law wasn't used and it doesn't matter if the gas is ideal or not. IDENTIFY: The type of process is not specified. We can use U = Q - W because this applies to all processes. Calculate U and then from it calculate T . SET UP: Q is positive since heat goes into the gas; Q = +1200 J W positive since gas expands; W = +2100 J EXECUTE: U = 1200 J - 2100 J = -900 J We can also use U = n ( 3 R ) T since this is true for any process for an ideal gas. 2 19.10. T = 2 U 2( -900 J) = = -14.4C 3nR 3(5.00 mol)(8.3145 J/mol K) 19.11. 19.12. T2 = T1 + T = 127C - 14.4C = 113C EVALUATE: More energy leaves the gas in the expansion work than enters as heat. The internal energy therefore decreases, and for an ideal gas this means the temperature decreases. We didn't have to convert T to kelvins since T is the same on the Kelvin and Celsius scales. IDENTIFY: Apply U = Q - W to the air inside the ball. SET UP: Since the volume decreases, W is negative. Since the compression is sudden, Q = 0. EXECUTE: U = Q - W with Q = 0 gives U = -W . W < 0 so U > 0. U = +410 J. (b) Since U > 0, the temperature increases. EVALUATE: When the air is compressed, work is done on the air by the force on the air. The work done on the air increases its energy. No energy leaves the gas as a flow of heat, so the internal energy increases. IDENTIFY and SET UP: Calculate W using the equation for a constant pressure process. Then use U = Q - W to calculate Q. (a) EXECUTE: 5 W = V2 V1 p dV = p(V2 - V1 ) for this constant pressure process. W = (2.3 10 Pa)(1.20 m3 - 1.70 m3 ) = -1.15 105 J (The volume decreases in the process, so W is negative.) (b) U = Q - W Q = U + W = -1.40 105 J + (-1.15 105 J) = -2.55 105 J Q negative means heat flows out of the gas. (c) EVALUATE: W = V2 V1 p dV = p(V2 - V1 ) (constant pressure) and U = Q - W apply to any system, not just to 19.13. an ideal gas. We did not use the ideal gas equation, either directly or indirectly, in any of the calculations, so the results are the same whether the gas is ideal or not. IDENTIFY: Calculate the total food energy value for one doughnut. K = 1 mv 2 . 2 SET UP: 1 cal = 4.186 J EXECUTE: (a) The energy is (2.0 g)(4.0 kcal g) + (17.0 g)(4.0 kcal g) + (7.0 g)(9.0 kcal g) = 139 kcal. The time required is (139 kcal) (510 kcal h) = 0.273 h = 16.4 min. (b) v = 2K m = 2(139 103 cal)(4.186 J cal) (60 kg) = 139 m s = 501 km h. EVALUATE: When we set K = Q, we must express Q in J, so we can solve for v in m/s. IDENTIFY: Apply U = Q - W . SET UP: W > 0 when the system does work. 19.14. 19-4 Chapter 19 19.15. 19.16. EXECUTE: (a) The container is said to be well-insulated, so there is no heat transfer. (b) Stirring requires work. The stirring needs to be irregular so that the stirring mechanism moves against the water, not with the water. (c) The work mentioned in part (b) is work done on the system, so W < 0, and since no heat has been transferred, U = -W > 0. EVALUATE: The stirring adds energy to the liquid and this energy stays in the liquid as an increase in internal energy. IDENTIFY: Apply U = Q - W to the gas. SET UP: For the process, V = 0. Q = +400 J since heat goes into the gas. EXECUTE: (a) Since V = 0, W = 0. p nR (b) pV = nRT says = = constant. Since p doubles, T doubles. Tb = 2Ta . T V (c) Since W = 0, U = Q = +400 J. U b = U a + 400 J. EVALUATE: For an ideal gas, when T increases, U increases. IDENTIFY: Apply U = Q - W . W is the area under the path in the pV-plane. SET UP: W > 0 when V increases. EXECUTE: (a) The greatest work is done along the path that bounds the largest area above the V-axis in the p-V plane, which is path 1. The least work is done along path 3. (b) W > 0 in all three cases; Q = U + W , so Q > 0 for all three, with the greatest Q for the greatest work, that along path 1. When Q > 0, heat is absorbed. EVALUATE: U is path independent and depends only on the initial and final states. W and Q are path independent and can have different values for different paths between the same initial and final states. IDENTIFY: U = Q - W . W is the area under the path in the pV-diagram. When the volume increases, W > 0. SET UP: For a complete cycle, U = 0. EXECUTE: (a) and (b) The clockwise loop (I) encloses a larger area in the p-V plane than the counterclockwise loop (II). Clockwise loops represent positive work and counterclockwise loops negative work, so WI > 0 and WII < 0. Over one complete cycle, the net work WI + WII > 0, and the net work done by the system is positive. (c) For the complete cycle, U = 0 and so W = Q. From part (a), W > 0, so Q > 0, and heat flows into the system. (d) Consider each loop as beginning and ending at the intersection point of the loops. Around each loop, U = 0, so Q = W ; then, QI = WI > 0 and QII = WII < 0. Heat flows into the system for loop I and out of the system for loop II. EVALUATE: W and Q are path dependent and are in general not zero for a cycle. IDENTIFY and SET UP: Deduce information about Q and W from the problem statement and then apply the first law, U = Q - W , to infer whether Q is positive or negative. EXECUTE: (a) For the water T > 0, so by Q = mc T heat has been added to the water. Thus heat energy comes from the burning fuel-oxygen mixture, and Q for the system (fuel and oxygen) is negative. (b) Constant volume implies W = 0. (c) The 1st law (Eq.19.4) says U = Q - W . Q < 0, W = 0 so by the 1st law U < 0. The internal energy of the fuel-oxygen mixture decreased. EVALUATE: In this process internal energy from the fuel-oxygen mixture was transferred to the water, raising its temperature. IDENTIFY: U = Q - W . For a constant pressure process, W = pV . SET UP: Q = +2.20 106 J; Q > 0 since this amount of heat goes into the water. p = 2.00 atm = 2.03 105 Pa. EXECUTE: (a) W = pV = (2.03 105 Pa)(0.824 m3 - 1.00 10-3 m3 ) = 1.67 105 J (b) U = Q - W = 2.20 106 J - 1.67 105 J = 2.03 106 J. EVALUATE: 2.20 106 J of energy enters the water. 1.67 105 J of energy leaves the materials through expansion work and the remainder stays in the material as an increase in internal energy. IDENTIFY: U = Q - W SET UP: Q < 0 when heat leaves the gas. EXECUTE: For an isothermal process, U = 0, so W = Q = -335 J. EVALUATE: In a compression the volume decreases and W < 0. 19.17. 19.18. 19.19. 19.20. The First Law of Thermodynamics 19-5 19.21. IDENTIFY: For a constant pressure process, W = pV , Q = nC p T and U = nCV T . U = Q - W and C p = CV + R. For an ideal gas, p V = nRT . SET UP: From Table 19.1, CV = 28.46 J/mol K. EXECUTE: (a) The pV diagram is given in Figure 19.21. (b) W = pV2 - pV1 = nR(T2 - T1 ) = (0.250 mol)(8.3145 J mol K)(100.0 K) = 208 J. (c) The work is done on the piston. (d) Since Eq. (19.13) holds for any process, U = nCV T = (0.250 mol)(28.46 J mol K)(100.0 K) = 712 J. (e) Either Q = nC p T or Q = U + W gives Q = 920 J to three significant figures. (f ) The lower pressure would mean a correspondingly larger volume, and the net result would be that the work done would be the same as that found in part (b). EVALUATE: W = nRT , so W, Q and U all depend only on T . When T increases at constant pressure, V increases and W > 0. U and Q are also positive when T increases. Figure 19.21 19.22. IDENTIFY: SET UP: For constant volume Q = nCV T . For constant pressure, Q = nC p T . For any process of an ideal R = 8.315 J/mol K. For helium, CV = 12.47 J/mol K and C p = 20.78 J/mol K. gas, U = nCV T . EXECUTE: (a) Q = nCV T = (0.0100 mol)(12.47 J mol K)(40.0 C) = 4.99 J. The pV-diagram is sketched in Figure 19.22a. (b) Q = nC p T = (0.0100 mol)(20.78 J/mol K)(40.0 C) = 8.31 J. The pV-diagram is sketched in Figure 19.22b. (c) More heat is required for the constant pressure process. U is the same in both cases. For constant volume W = 0 and for constant pressure W > 0. The additional heat energy required for constant pressure goes into expansion work. (d) U = nCV T = 4.99 J for both processes. U is path independent and for an ideal gas depends only on T . EVALUATE: C p = CV + R, so C p > CV . Figure 19.22 19.23. IDENTIFY: SET UP: For constant volume, Q = nCV T . For constant pressure, Q = nC p T . From Table 19.1, CV = 20.76 J/mol K and C p = 29.07 J/mol K Q 645 J = = 167.9 K and T = 948 K. nCV (0.185 mol)(20.76 J mol K) EXECUTE: (a) Using Equation (19.12), T = The pV-diagram is sketched in Figure 19.23a. 19-6 Chapter 19 (b) Using Equation (19.14), T = 645 J Q = = 119.9 K and T = 900 K. nC p (0.185 mol)(29.07 J mol K) The pV-diagram is sketched in Figure 19.23b. EVALUATE: At constant pressure some of the heat energy added to the gas leaves the gas as expansion work and the internal energy change is less than if the same amount of heat energy is added at constant volume. T is proportional to U . Figure 19.23 19.24. IDENTIFY and SET UP: Use information about the pressure and volume in the ideal gas law to determine the sign of T , and from that the sign of Q. EXECUTE: For constant p, Q = nC p T Since the gas is ideal, pV = nRT and for constant p, p V = nR T . p V Q = nC p nR Cp p V = R Since the gas expands, V > 0 and therefore Q > 0. Q > 0 means heat goes into gas. EVALUATE: Heat flows into the gas, W is positive and the internal energy increases. It must be that Q > W . 19.25. IDENTIFY: SET UP: EXECUTE: U = Q - W . For an ideal gas, U = CV T , and at constant pressure, W = p V = nR T . CV = 3 R for a monatomic gas. 2 3 U = n( 3 R ) T = 3 p V = 2 W . Then Q = U + W = 5 W , so W Q = 2 . 5 2 2 2 19.26. EVALUATE: For diatomic or polyatomic gases, CV is a different multiple of R and the fraction of Q that is used for expansion work is different. IDENTIFY: For an ideal gas, U = CV T , and at constant pressure, pV = nRT . SET UP: EXECUTE: EVALUATE: CV = 3 R for a monatomic gas. 2 3 U = n ( 3 R ) T = 3 pV = 2 (4.00 104 Pa)(8.00 10-3 m3 - 2.00 10-3 m3 ) = 360 J. 2 2 5 W = nRT = 2 U = 240 J. Q = nC p T = n( 5 R ) T = 3 U = 600 J. 600 J of heat energy flows into 3 2 19.27. the gas. 240 J leaves as expansion work and 360 J remains in the gas as an increase in internal energy. IDENTIFY: For a constant volume process, Q = nCV T . For a constant pressure process, Q = nC p T . For any process of an ideal gas, U = nCV T . SET UP: From Table 19.1, for N 2 , CV = 20.76 J/mol K and C p = 29.07 J/mol K. Heat is added, so Q is Q 1557 J = = +25.0 K nCV (3.00 mol)(20.76 J/mol K) positive and Q = +1557 J. EXECUTE: (a) T = (b) T = Q 1557 J = = +17.9 K nC p (3.00 mol)(29.07 J/mol K) (c) U = nCV T for either process, so U is larger when T is larger. The final internal energy is larger for the constant volume process in (a). EVALUATE: For constant volume W = 0 and all the energy added as heat stays in the gas as internal energy. For the constant pressure process the gas expands and W > 0. Part of the energy added as heat leaves the gas as expansion work done by the gas. The First Law of Thermodynamics 19-7 19.28. IDENTIFY: Apply pV = nRT to calculate T. For this constant pressure process, W = pV . Q = nC p T . Use U = Q - W to relate Q, W and U . SET UP: 2.50 atm = 2.53 105 Pa. For a monatomic ideal gas, CV = 12.47 J/mol K and C p = 20.78 J/mol K. EXECUTE: (a) T1 = pV1 (2.53 105 Pa)(3.20 10-2 m 2 ) = = 325 K. nR (3.00 mol)(8.314 J/mol K) T2 = pV2 (2.53 105 Pa)(4.50 10-2 m 2 ) = = 456 K. nR (3.00 mol)(8.314 J/mol K) (b) W = pV = (2.53 105 Pa)(4.50 10-2 m3 - 3.20 10 -2 m3 ) = 3.29 103 J (c) Q = nC p T = (3.00 mol)(20.78 J/mol K)(456 K - 325 K) = 8.17 103 J (d) U = Q - W = 4.88 103 J EVALUATE: We could also calculate U as U = nCV T = (3.00 mol)(12.47 J/mol K)(456 K - 325 K) = 4.90 103 J, which agrees with the value we calculated in part (d). IDENTIFY: Calculate W and U and then use the first law to calculate Q. (a) SET UP: 19.29. W = V2 V1 p dV pV = nRT so p = nRT / V W = (nRT / V ) dV = nRT dV / V = nRT ln(V2 / V1 ) (work done during an isothermal process). V1 V1 V2 V2 EXECUTE: W = (0.150 mol)(8.3145 J/mol K)(350 K)ln(0.25V1 / V1 ) = (436.5 J)ln(0.25) = -605 J. EVALUATE: W for the gas is negative, since the volume decreases. (b) EXECUTE: U = nCV T for any ideal gas process. T = 0 (isothermal) so U = 0. EVALUATE: U = 0 for any ideal gas process in which T doesn't change. (c) EXECUTE: U = Q - W U = 0 so Q = W = -605 J. (Q is negative; the gas liberates 605 J of heat to the surroundings.) EVALUATE: Q = nCV T is only for a constant volume process so doesn't apply here. Cp CV Q = nC p T is only for a constant pressure process so doesn't apply here. 19.30. IDENTIFY: SET UP: EXECUTE: C p = CV + R and = . R = 8.315 J/mol K C p = CV + R. = Cp CV =1+ R R 8.315 J/mol K = = 65.5 J/mol K. Then . CV = CV 0.127 -1 C p = CV + R = 73.8 J/mol K. 19.31. EVALUATE: The value of CV is about twice the values for the polyatomic gases in Table 19.1. A propane molecule has more atoms and hence more internal degrees of freedom than the polyatomic gases in the table. IDENTIFY: U = Q - W . Apply Q = nC p T to calculate C p . Apply U = nCV T to calculate CV . = C p / CV . SET UP: T = 15.0 C = 15.0 K. Since heat is added, Q = +970 J. EXECUTE: (a) U = Q - W = +970 J - 223 J = 747 J (b) C p = Q 970 J U 747 J = = 37.0 J/mol K. CV = = = 28.5 J/mol K. nT (1.75 mol)(15.0 K) nT (1.75 mol)(15.0 K) 19.32. 37.0 J/mol K = 1.30 28.5 J/mol K EVALUATE: The value of we calculated is similar to the values given in Tables 19.1 for polyatomic gases. IDENTIFY and SET UP: For an ideal gas U = nCV T . The sign of U is the same as the sign of T . Combine Eq.(19.22) and the ideal gas law to obtain an equation relating T and p, and use it to determine the sign of T . 1 EXECUTE: TV1 -1 = T2V2 -1 and V = nRT / p so, T1 p1 - = T2 p1- and T2 = T1 ( p2 / p1 ) -1 1 2 = Cp CV = p2 < p1 and - 1 is positive so T2 < T1. T is negative so U is negative; the energy of the gas decreases. EVALUATE: Eq.(19.24) shows that the volume increases for this process, so it is an adiabatic expansion. In an adiabatic expansion the temperature decreases. 19-8 Chapter 19 19.33. IDENTIFY: SET UP: For an adiabatic process of an ideal gas, p1V1 = p2V2 , W = For a monatomic ideal gas = 5/ 3. 5/3 1 ( p1V1 - p2V2 ) and TV1 -1 = T2V2 -1. 1 -1 V 0.0800 m3 5 EXECUTE: (a) p2 = p1 1 = (1.50 105 Pa ) = 4.76 10 Pa. V2 0.0400 m3 (b) This result may be substituted into Eq.(19.26), or, substituting the above form for p2 , W= 0.0800 2 / 3 1 3 -1 4 p1V1 1 - (V1 / V2 ) = (1.50 105 Pa )( 0.0800 m3 ) 1 - = -1.06 10 J. 0.0400 2 -1 ( ) (c) From Eq.(19.22), (T2 T1 ) = (V2 V1 ) -1 = ( 0.0800 0.0400 ) 23 = 1.59, and since the final temperature is higher than 19.34. the initial temperature, the gas is heated. EVALUATE: In an adiabatic compression W < 0 since V < 0. Q = 0 so U = -W . U > 0 and the temperature increases. IDENTIFY and SET UP: (a) In the process the pressure increases and the volume decreases. The pV-diagram is sketched in Figure 19.34. Figure 19.34 (b) For an adiabatic process for an ideal gas TV1 -1 = T2V2 -1 , p1V1 = p2V2 , and pV = nRT 1 EXECUTE: From the first equation, T2 = T1 (V1 / V2 ) -1 = (293 K)(V1 / 0.0900V1 )1.4 -1 T2 = (293 K)(11.11)0.4 = 768 K = 495C (Note: In the equation TV1 -1 = T2V2 -1 the temperature must be in kelvins.) 1 p1V1 = p2V2 implies p2 = p1 (V1 / V2 ) = (1.00 atm)(V1 / 0.0900V1 )1.4 p2 = (1.00 atm)(11.11)1.4 = 29.1 atm EVALUATE: Alternatively, we can use pV = nRT to calculate p2 : n, R constant implies pV / T = nR = constant so p1V1 / T1 = p2V2 / T2 p2 = p1 (V1 / V2 )(T2 / T1 ) = (1.00 atm)(V1 / 0.0900V1 )(768 K/293 K) = 29.1 atm, which checks. 19.35. IDENTIFY: SET UP: For an adiabatic process of an ideal gas, W = 1 ( p1V1 - p2V2 ) and p1V1 = p2V2 . -1 = 1.40 for an ideal diatomic gas. 1 atm = 1.013 105 Pa and 1 L = 10-3 m3 . 1 EXECUTE: Q = U + W = 0 for an adiabatic process, so U = -W = ( p2V2 - p1V1 ) . p1 = 1.22 105 Pa. -1 p2 = p1 (V1 / V2 ) = (1.22 105 Pa)(3)1.4 = 5.68 105 Pa. 1 ([5.68 105 Pa][10 10-3 m -3 ] - [1.22 105 Pa][30 10-3 m -3 ]) = 5.05 103 J. The internal energy 0.40 increases because work is done on the gas ( U > 0) and Q = 0. The temperature increases because the internal energy has increased. EVALUATE: In an adiabatic compression W < 0 since V < 0. Q = 0 so U = -W . U > 0 and the temperature increases. IDENTIFY: Assume the expansion is adiabatic. TV1 -1 = T2V2 -1 relates V and T. Assume the air behaves as an ideal 1 W= gas, so U = nCV T . Use pV = nRT to calculate n. SET UP: 19.36. For air, CV = 29.76 J/mol K and = 1.40. V2 = 0.800V1. T1 = 293.15 K. p1 = 2.026 105 Pa. For a sphere, V = 4 r 3 . 3 The First Law of Thermodynamics 19-9 V V1 EXECUTE: (a) T2 = T1 1 = (293.15 K) = 320.5 K = 47.4C. V2 0.800V1 p V (2.026 105 Pa)(7.15 10-3 m3 ) 4 = 0.594 mol. (b) V1 = 4 r 3 = (0.1195 m)3 = 7.15 10-3 m3 . n = 1 1 = 3 RT1 (8.314 J/mol K)(293.15 K) 3 U = nCV T = (0.594 mol)(20.76 J/mol K)(321 K - 293 K) = 345 J. 1 EVALUATE: We could also use U = W = ( p1V1 - p2V2 ) to calculate U , if we first found p2 from pV = nRT . -1 (a) IDENTIFY and SET UP: In the expansion the pressure decreases and the volume increases. The pV-diagram is sketched in Figure 19.37. -1 0.40 19.37. Figure 19.37 (b) Adiabatic means Q = 0. Then U = Q - W gives W = -U = - nCV T = nCV (T1 - T2 ) (Eq.19.25). CV = 12.47 J/mol K (Table 19.1) EXECUTE: W = (0.450 mol)(12.47 J/mol K)(50.0C - 10.0C) = +224 J W positive for V > 0 (expansion) (c) U = -W = -224 J. EVALUATE: There is no heat energy input. The energy for doing the expansion work comes from the internal energy of the gas, which therefore decreases. For an ideal gas, when T decreases, U decreases. IDENTIFY: pV = nRT . For an adiabatic process, TV1 -1 = T2V2 -1. 1 SET UP: For an ideal monatomic gas, = 5/ 3. pV (1.00 105 Pa) (2.50 10-3 m3 ) EXECUTE: (a) T = = = 301 K. nR (0.1 mol) (8.3145 J mol K ) (b) (i) Isothermal: If the expansion is isothermal, the process occurs at constant temperature and the final temperature is the same as the initial temperature, namely 301 K. p2 = p1 (V1 / V2 ) = 1 p1 = 5.00 104 Pa. 2 19.38. (ii) Isobaric: p = 0 so p2 = 1.00 105 Pa. T2 = T1 (V2 / V1 ) = 2T1 = 602 K. 0.67 TV1 -1 (301 K)(V1 ) 0.67 1 = = (301 K) ( 1 ) = 189 K. 2 V2 -1 (2V1 ) 0.67 EVALUATE: In an isobaric expansion, T increases. In an adiabatic expansion, T decreases. IDENTIFY: Combine TV1 -1 = T2V2 -1 with pV = nRT to obtain an expression relating T and p for an adiabatic 1 process of an ideal gas. SET UP: T1 = 299.15 K (iii) Adiabatic: Using Equation (19.22), T2 = 19.39. EXECUTE: nRT1 nRT V= so T1 p p1 ( -1) / -1 nRT2 = T2 p2 -1 and T1 p1 -1 = T2 p2 -1 . 19.40. p 0.850 105 Pa T2 = T1 2 = (299.15 K) = 284.8 K = 11.6 C 5 1.01 10 Pa p1 EVALUATE: For an adiabatic process of an ideal gas, when the pressure decreases the temperature decreases. IDENTIFY: Apply U = Q - W . For any process of an ideal gas, U = nCV T . For an isothermal expansion, V p W = nRT ln 2 = nRT ln 1 . V1 p2 p V SET UP: T = 288.15 K. 1 = 2 = 2.00. p2 V1 EXECUTE: (a) U = 0 since T = 0. (b) W = (1.50 mol)(8.314 J/mol K)(288.15 K) ln(2.00) = 2.49 103 J. W > 0 and work is done by the gas. Since U = 0, Q = W = +2.49 103 J. Q > 0 so heat flows into the gas. EVALUATE: When the volume increases, W is positive. 0.4 /1.4 19-10 Chapter 19 19.41. IDENTIFY and SET UP: For an ideal gas, pV = nRT . The work done is the area under the path in the pV-diagram. EXECUTE: (a) The product pV increases and this indicates a temperature increase. (b) The work is the area in the pV plane bounded by the blue line representing the process and the verticals at Va and Vb . The area of this trapezoid is 1 ( pb + pa )(Vb - Va ) = 1 (2.40 105 Pa)(0.0400 m 3 ) = 4800 J. 2 2 19.42. EVALUATE: The work done is the average pressure, 1 ( p1 + p2 ), times the volume increase. 2 IDENTIFY: Use pV = nRT to calculate T. W is the area under the process in the pV-diagram. Use U = nCV T and U = Q - W to calculate Q. SET UP: In state c, pc = 2.0 105 Pa and Vc = 0.0040 m3 . In state a, pa = 4.0 105 Pa and Va = 0.0020 m 3 . EXECUTE: (a) Tc = pcVc (2.0 105 Pa)(0.0040 m3 ) = = 192 K nR (0.500 mol)(8.314 J/mol K) 19.43. (b) W = 1 (4.0 105 Pa + 2.0 105 Pa)(0.0030 m 3 - 0.0020 m3 ) + (2.0 105 Pa)(0.0040 m3 - 0.0030 m 3 ) 2 W = +500 J. 500 J of work is done by the gas. pV (4.0 105 Pa)(0.0020 m3 ) (c) Ta = a a = = 192 K. For the process, T = 0, so U = 0 and Q = W = +500 J. nR (0.500 mol)(8.314 J/mol K) 500 J of heat enters the system. EVALUATE: The work done by the gas is positive since the volume increases. IDENTIFY: Use U = Q - W and the fact that U is path independent. W > 0 when the volume increases, W < 0 when the volume decreases, and W = 0 when the volume is constant. Q > 0 if heat flows into the system. SET UP: The paths are sketched in Figure 19.43. Qacb = +90.0 J (positive since heat flows in) Wacb = +60.0 J (positive since V > 0) Figure 19.43 EXECUTE: (a) U = Q - W U is path independent; Q and W depend on path. the U = U b - U a This can be calculated for any path from a to b, in particular for path acb: U a b = Qacb - Wacb = 90.0 J - 60.0 J = 30.0 J. Now apply U = Q - W to path adb; U = 30.0 J for this path also. Wadb = +15.0 J (positive since V > 0) U a b = Qadb - Wadb so Qacb = U a b + Wadb = 30.0 J + 15.0 J = +45.0 J (b) Apply U = Q - W to path ba: U b a = Qba - Wba Wba = -35.0 J (negative since V < 0) U b a = U a - U b = -(U b - U a ) = -U a b = -30.0 J Then Qba = U b a + Wba = -30.0 J - 35.0 J = -65.0 J. (Qba < 0; the system liberates heat.) (c) U a = 0, U d = 8.0 J U a b = U b - U a = +30.0 J, so U b = +30.0 J. process a d U a d = Qad - Wad U a d = U d - U a = +8.0 J Wadb = +15.0 J and Wadb = Wad + Wdb . But the work Wdb for the process d b is zero since V = 0 for that process. Therefore Wad = Wadb = +15.0 J. Then Qad = U a d + Wad = +8.0 J + 15.0 J = +23.0 J (positive implies heat absorbed). The First Law of Thermodynamics 19-11 process d b U d b = Qdb - Wdb Wdb = 0, as already noted. U d b = U b - U d = 30.0 J - 8.0 J = +22.0 J. Then Qdb = U d b + Wdb = +22.0 J (positive; heat absorbed). EVALUATE: The signs of our calculated Qad and Qdb agree with the problem statement that heat is absorbed in these processes. IDENTIFY: U = Q - W . SET UP: W = 0 when V = 0. EXECUTE: For each process, Q = U + W . No work is done in the processes ab and dc, and so Wbc = Wabc = 450 J 19.44. and Wad = Wadc = 120 J. The heat flow for each process is: for ab, Q = 90 J. For bc, Q = 440 J + 450 J = 890 J. For ad , Q = 180 J + 120 J = 300 J. For dc, Q = 350 J. Heat is absorbed in each process. Note that the arrows representing the processes all point in the direction of increasing temperature (increasing U ). EVALUATE: U is path independent so is the same for paths adc and abc. Qadc = 300 J + 350 J = 650 J. Qabc = 90 J + 890 J = 980 J. Q and W are path dependent and are different for these two paths. 19.45. IDENTIFY: Use pV = nRT to calculate Tc / Ta . Calculate U and W and use U = Q - W to obtain Q. SET UP: For path ac, the work done is the area under the line representing the process in the pV-diagram. T pV (1.0 105 J)(0.060 m3 ) EXECUTE: (a) c = c c = = 1.00. Tc = Ta . Ta paVa (3.0 105 J)(0.020 m3 ) (b) Since Tc = Ta , U = 0 for process abc. For ab, V = 0 and Wab = 0. For bc, p is constant and Wbc = pV = (1.0 105 Pa)(0.040 m 3 ) = 4.0 103 J. Therefore, Wabc = +4.0 103 J. Since U = 0, Q = W = +4.0 103 J. 4.0 103 J of heat flows into the gas during process abc. 19.46. (c) W = 1 (3.0 105 Pa + 1.0 105 Pa)(0.040 m 3 ) = +8.0 103 J. Qac = Wac = +8.0 103 J. 2 EVALUATE: The work done is path dependent and is greater for process ac than for process abc, even though the initial and final states are the same. IDENTIFY: For a cycle, U = 0 and Q = W . Calculate W. SET UP: The magnitude of the work done by the gas during the cycle equals the area enclosed by the cycle in the pV-diagram. EXECUTE: (a) The cycle is sketched in Figure 19.46. (b) W = (3.50 104 Pa - 1.50 104 Pa)(0.0435 m3 - 0.0280 m3 ) = +310 J. More negative work is done for cd than positive work for ab and the net work is negative. W = -310 J. (c) Q = W = -310 J. Since Q < 0, the net heat flow is out of the gas. EVALUATE: During each constant pressure process W = pV and during the constant volume process W = 0. Figure 19.46 19.47. IDENTIFY: Use the 1st law to relate Qtot to Wtot for the cycle. Calculate Wab and Wbc and use what we know about Wtot to deduce Wca 19-12 Chapter 19 (a) SET UP: We aren't told whether the pressure increases or decreases in process bc. The two possibilities for the cycle are sketched in Figure 19.47. Figure 19.47 In cycle I, the total work is negative and in cycle II the total work is positive. For a cycle, U = 0, so Qtot = Wtot The net heat flow for the cycle is out of the gas, so heat Qtot < 0 and Wtot < 0. Sketch I is correct. (b) EXECUTE: Wtot = Qtot = -800 J Wtot = Wab + Wbc + Wca Wbc = 0 since V = 0. Wab = pV since p is constant. But since it is an ideal gas, pV = nRT Wab = nR(Tb - Ta ) = 1660 J Wca = Wtot - Wab = -800 J - 1660 J = -2460 J EVALUATE: In process ca the volume decreases and the work W is negative. IDENTIFY: Apply the appropriate expression for W for each type of process. pV = nRT and C p = CV + R. SET UP: R = 8.315 J/mol K EXECUTE: Path ac has constant pressure, so Wac = pV = nRT , and Wac = nR(Tc - Ta ) = (3 mol)(8.3145 J mol K)(492 K - 300 K) = 4.789 103 J. 19.48. Path cb is adiabatic (Q = 0), so Wcb = Q - U = -U = -nCV T , and using CV = C p - R, Wcb = -n(C p - R)(Tb - Tc ) = -(3 mol)(29.1 J mol K - 8.3145 J mol K)(600 K - 492 K) = -6.735 103 J. Path ba has constant volume, so Wba = 0. So the total work done is W = Wac + Wcb + Wba = 4.789 103 J - 6.735 103 J + 0 = -1.95 103 J. EVALUATE: W > 0 when V > 0, W < 0 when V < 0 and W = 0 when V = 0. IDENTIFY: Use Q = nCV T to calculate the temperature change in the constant volume process and use pV = nRT to calculate the temperature change in the constant pressure process. The work done in the constant 19.49. volume process is zero and the work done in the constant pressure process is W = pV . Use Q = nC p T to calculate the heat flow in the constant pressure process. U = nCV T , or U = Q - W . SET UP: For N 2 , CV = 20.76 J/mol K and C p = 29.07 J/mol K. EXECUTE: (a) For process ab, T = Q 1.52 104 J = = 293 K. Ta = 293 K, so Tb = 586 K. nCV (2.50 mol)(20.76 J/mol K) pV = nRT says T doubles when V doubles and p is constant, so Tc = 2(586 K) = 1172 K = 899C. (b) For process ab, Wab = 0. For process bc, Wbc = pV = nRT = (2.50 mol)(8.314 J/mol K)(1172 K - 586 K) = 1.22 104 J. W = Wab + Wbc = 1.22 104 J. (c) For process bc, Q = nC p T = (2.50 mol)(29.07 J/mol K)(1172 K - 586 K) = 4.26 10 4 J. (d) U = nCV T = (2.50 mol)(20.76 J/mol K)(1172 K - 293 K) = 4.56 10 4 J. EVALUATE: The total Q is 1.52 104 J + 4.26 10 4 J = 5.78 104 J. U = Q - W = 5.78 104 J - 1.22 104 J = 4.56 10 4 J, which agrees with our results in part (d). 19.50. IDENTIFY: SET UP: For a constant pressure process, Q = nC p T . U = Q - W . U = nCV T for any ideal gas process. For N 2 , CV = 20.76 J/mol K and C p = 29.07 J/mol K. Q < 0 if heat comes out of the gas. EXECUTE: (a) n = Q +2.5104 J = = 21.5 mol. C p T (29.07 J mol K)(40.0 K) (b) U = nCV T = Q(CV / C p ) = ( -2.5 104 J)(20.76/29.07) = -1.79 104 J. The First Law of Thermodynamics 19-13 (c) W = Q - U = -7.15 103 J. (d) U is the same for both processes, and if V = 0, W = 0 and Q = U = -1.79 104 J. EVALUATE: For a given T , Q is larger when the pressure is constant than when the volume is constant. IDENTIFY and SET UP: Use the first law to calculate W and then use W = pV for the constant pressure process to calculate V . EXECUTE: U = Q - W Q = -2.15 105 J (negative since heat energy goes out of the system) 19.51. U = 0 so W = Q = -2.15 105 J Constant pressure, so W = Then V = V2 V1 pdV = p (V2 - V1 ) = pV . 19.52. W -2.15 105 J = = -0.226 m3 . p 9.50 105 Pa EVALUATE: Positive work is done on the system by its surroundings; this inputs to the system the energy that then leaves the system as heat. Both Eq.(19.4) and (19.2) apply to all processes for any system, not just to an ideal gas. IDENTIFY: pV = nRT . For an isothermal process W = nRT ln(V2 / V1 ). For a constant pressure process, W = p V . SET UP: 1 L = 10-3 m3 . EXECUTE: (a) The pV-diagram is sketched in Figure 19.52. 1.00 105 Pa (b) At constant temperature, the product pV is constant, so V2 = V1 ( p1 / p2 ) = (1.5 L) = 6.00 L. The 4 2.50 10 Pa final pressure is given as being the same as p3 = p2 = 2.5 104 Pa. The final volume is the same as the initial volume, so T3 = T1 ( p3 p1 ) = 75.0 K. (c) Treating the gas as ideal, the work done in the first process is W = nRT ln(V2 V1 ) = p1V1 ln( p1 p2 ). 1.00 105 Pa W = (1.00 105 Pa)(1.5 10-3 m3 )ln = 208 J. 4 2.50 10 Pa For the second process, W = p2 (V3 - V2 ) = p2 (V1 - V2 ) = p2V1 (1 - ( p1 p2 )). 1.00 105 Pa W = (2.50 104 Pa)(1.5 10-3 m3 ) 1 - = -113 J. 4 2.50 10 Pa The total work done is 208 J - 113 J = 95 J. (d) Heat at constant volume. No work would be done by the gas or on the gas during this process. EVALUATE: When the volume increases, W > 0. When the volume decreases, W < 0. Figure 19.52 19.53. IDENTIFY: V = V0 T . W = pV since the force applied to the piston is constant. Q = mc p T . U = Q - W . SET UP: m = V EXECUTE: (a) The fractional change in volume is V = V0 T = (1.20 10 -2 m3 )(1.20 10 -3 K -1 )(30.0 K) = 4.32 10 -4 m3 . (b) W = pV = ( F A) V = ((3.00 104 N) (0.0200 m 2 ))(4.32 10-4 m 3 ) = 648 J. (c) Q = mc p T = V0 c p T = (1.20 10-2 m3 )(791 kg m3 )(2.51 103 J kg K)(30.0 K). Q = 7.15 105 J. 19-14 Chapter 19 (d) U = Q - W = 7.15 105 J to three figures. (e) Under these conditions W is much less than Q and there is no substantial difference between cV and c p . EVALUATE: 19.54. IDENTIFY: U = Q - W . U = Q - W is valid for any material. For liquids the expansion work is much less than Q. V = V0 T . W = pV since the applied pressure (air pressure) is constant. Q = mc p T . For copper, = 5.1 10-3 (C)-1 , c p = 390 J/kg K and = 8.90 103 kg/m 3 . SET UP: EXECUTE: (a) V = TV0 = (5.1 10-5 (C) -1 )(70.0 C)(2.00 10-2 m)3 = 2.86 10-8 m 3 . (b) W = pV = 2.88 10 -3 J. (c) Q = mc p T = V0c p T = (8.9 103 kg m3 )(8.00 10-6 m3 )(390 J kg K)(70.0 C) = 1944 J. (d) To three figures, U = Q = 1940 J. (e) Under these conditions, the difference is not substantial, since W is much less than Q. EVALUATE: U = Q - W applies to any material. For solids the expansion work is much less than Q. 19.55. IDENTIFY and SET UP: The heat produced from the reaction is Qreaction = mLreaction , where Lreaction is the heat of reaction of the chemicals. Qreaction = W + U spray EXECUTE: For a mass m of spray, W = 1 mv 2 = 1 m(19 m/s) 2 = (180.5 J/kg)m and 2 2 U spray = Qspray = mcT = m(4190 J/kg K)(100C - 20C) = (335,200 J/kg)m. Then Qreaction = (180 J/kg + 335, 200 J/kg)m = (335,380 J/kg)m and Qreaction = mLreaction implies mLreaction = (335,380 J/kg)m. The mass m divides out and Lreaction = 3.4 105 J/kg EVALUATE: The amount of energy converted to work is negligible for the two significant figures to which the answer should be expressed. Almost all of the energy produced in the reaction goes into heating the compound. IDENTIFY: The process is adiabatic. Apply p1V1 = p2V2 and pV = nRT . Q = 0 so U = -W = - SET UP: 19.56. 1 ( p1V1 - p2V2 ). -1 For helium, = 1.67. p1 = 1.00 atm = 1.013 105 Pa. V1 = 2.00 103 m 3 . 1/ p2 = 0.900 atm = 9.117 104 Pa. T1 = 288.15 K. p p EXECUTE: (a) V2 = V1 1 . V2 = V1 1 p2 p2 T T (b) pV = nRT gives 1 = 2 . p1V1 p2V2 1.00 atm = (2.00 103 m3 ) 0.900 atm 1/1.67 = 2.13 103 m3 . 19.57. 3 3 p V 0.900 atm 2.13 10 m T2 = T1 2 2 = (288.15 K) = 276.2 K = 3.0C. 3 3 1.00 atm 2.00 10 m p1 V1 1 (c) U = - ([1.013 105 Pa)(2.00 103 m3 )] - [9.117 104 Pa)(2.13 103 m3 )] = -1.25 107 J. 0.67 EVALUATE: The internal energy decreases when the temperature decreases. IDENTIFY: For an adiabatic process of an ideal gas, TV1 -1 = T2V2 -1. pV = nRT . 1 SET UP: For air, = 1.40 = 7 . 5 EXECUTE: (a) As the air moves to lower altitude its density increases; under an adiabatic compression, the temperature rises. If the wind is fast-moving, Q is not as likely to be significant, and modeling the process as adiabatic (no heat loss to the surroundings) is more accurate. nRT 1 (b) V = , so TV1 -1 = T2V2 -1 gives T1 p1 - = T2 p1- . The temperature at the higher pressure is 1 2 p T2 = T1 ( p1 / p2 ) ( -1) / = (258.15 K) ([8.12 104 Pa]/[5.60 104 Pa]) 2/7 = 287.1 K = 13.0C so the temperature would rise by 11.9 C. EVALUATE: In an adiabatic compression, Q = 0 but the temperature rises because of the work done on the gas. The First Law of Thermodynamics 19-15 19.58. IDENTIFY: For constant pressure , W = pV . For an adiabatic process of an ideal gas, W = CV ( p1V1 - p2V2 ) and R p1V1 = p2V2 . R CV CV CV EXECUTE: (a) The pV-diagram is sketched in Figure 19.58. C (b) The work done is W = p0 (2V0 - V0 ) + V ( p0 (2V0 ) - p3 (4V0 )). p3 = p0 (2V0 4V0 ) and so R C W = p0V0 1 + V (2 - 22 - ) . Note that p0 is the absolute pressure. R (c) The most direct way to find the temperature is to find the ratio of the final pressure and volume to the original SET UP: = Cp = C p + CV =1+ V V and treat the air as an ideal gas. p3 = p2 2 = p1 2 , since p1 = p2 . Then V3 V3 V V p3V3 2 - 1 = T0 2 3 = T0 4 = T0 ( 2 ) . p1V1 V3 V1 2 p0V0 pV C (d) Since n = , Q = 0 0 ( CV + R )( 2T0 - T0 ) = p0V0 V + 1 . This amount of heat flows into the gas, since RT0 RT0 R Q > 0. EVALUATE: In the isobaric expansion the temperature doubles and in the adiabatic expansion the temperature decreases. If the gas is diatomic, with = 7 , 2 - = 3 and T3 = 3.03T0 , W = 2.21 p0V0 and Q = 3.50 p0V0 . 5 5 T3 = T0 U = 1.29 p0V0 . U > 0 and this is consistent with an increase in temperature. Figure 19.58 19.59. IDENTIFY: Assume that the gas is ideal and that the process is adiabatic. Apply Eqs.(19.22) and (19.24) to relate pressure and volume and temperature and volume. The distance the piston moves is related to the volume of the gas. Use Eq.(19.25) to calculate W. (a) SET UP: = C p / CV = (CV + R ) / CV = 1 + R / CV = 1.40. The two positions of the piston are shown in Figure 19.59. p1 = 1.01 105 Pa p2 = 4.20 105 Pa + pair = 5.21 106 Pa V1 = h1 A V2 = h2 A Figure 19.59 EXECUTE: adiabatic process: p1V1 = p2V2 p1h1 A = p2 h2 A p 1.01 105 Pa h2 = h1 1 = (0.250 m) = 0.0774 m 5 5.21 10 Pa p2 The piston has moved a distance h1 - h2 = 0.250 m - 0.0774 m = 0.173 m. 1/ 1/1.40 19-16 Chapter 19 (b) TV1 -1 = T2V2 -1 1 T1h1 -1 A -1 = T2 h2 -1 A -1 h 0.250 m T2 = T1 1 = 300.1 K 0.0774 m h2 (c) W = nCV (T1 - T2 ) (Eq.19.25) -1 0.40 = 479.7 K = 207C 19.60. W = (20.0 mol)(20.8 J/mol K)(300.1 K - 479.7 K) = -7.47 104 J EVALUATE: In an adiabatic compression of an ideal gas the temperature increases. In any compression the work W is negative. pM IDENTIFY: m = V . The density of air is given by = . For an adiabatic process, TV1 -1 = T2V2 -1. 1 RT pV = nRT nRT 1 in TV1 -1 = T2V2 -1 gives T1 p1 - = T2 p1- . 1 2 p EXECUTE: (a) The pV-diagram is sketched in Figure 19.60. (b) The final temperature is the same as the initial temperature, and the density is proportional to the absolute pressure. The mass needed to fill the cylinder is then SET UP: Using V = m = p0V p 1.45 105 Pa = (1.23 kg/m3 )(575 10-6 m3 ) = 1.02 10-3 kg. pair 1.01 105 Pa Without the turbocharger or intercooler the mass of air at T = 15.0C and p = 1.01 105 Pa in a cylinder is m = 0V = 7.07 10-4 kg. The increase in power is proportional to the increase in mass of air in the cylinder; the percentage increase is 1.02 10-3 kg - 1 = 0.44 = 44%. 7.07 10-4 kg ( -1) / p (c) The temperature after the adiabatic process is T2 = T1 2 p1 T p p = 0 1 2 = 0 2 T2 p1 p1 (1- ) / . The density becomes p2 p2 = 0 p1 p1 1/ . The mass of air in the cylinder is 1 1.40 1.45 105 Pa m = (1.23 kg/m3 )(575 10 -6 m3 ) 5 1.01 10 Pa = 9.16 10-4 kg, 9.16 10-4 kg - 1 = 0.30 = 30%. 7.07 10-4 kg EVALUATE: The turbocharger and intercooler each have an appreciable effect on the engine power. The percentage increase in power is Figure 19.60 19.61. IDENTIFY: In each case calculate either U or Q for the specific type of process and then apply the first law. (a) SET UP: isothermal ( T = 0) U = Q - W ; W = +300 J For any process of an ideal gas, U = nCV T . EXECUTE: Therefore, for an ideal gas, if T = 0 then U = 0 and Q = W = +300 J. (b) SET UP: adiabatic (Q = 0) U = Q - W ; W = +300 J EXECUTE: Q = 0 says U = -W = -300 J The First Law of Thermodynamics 19-17 (c) SET UP: isobaric p = 0 Use W to calculate T and then calculate Q. EXECUTE: W = pT = nRT ; T = W / nR Q = nC p T and for a monatomic ideal gas C p = 5 R 2 Thus Q = n 5 RT = (5Rn/2)(W/nR) = 5W/2 = +750 J. 2 U = nCV T for any ideal gas process and CV = C p - R = 3 R. 2 Thus U = 3W / 2 = +450 J EVALUATE: 300 J of energy leaves the gas when it performs expansion work. In the isothermal process this energy is replaced by heat flow into the gas and the internal energy remains the same. In the adiabatic process the energy used in doing the work decreases the internal energy. In the isobaric process 750 J of heat energy enters the gas, 300 J leaves as the work done and 450 J remains in the gas as increased internal energy. IDENTIFY: pV = nRT . For the isobaric process, W = pV = nRT . For the isothermal process, V W = nRT ln f . Vi SET UP: R = 8.315 J/mol K EXECUTE: (a) The pV diagram for these processes is sketched in Figure 19.62. T p T T (b) Find T2 . For process 1 2, n, R, and p are constant so = = constant. 1 = 2 and V nR V1 V2 V T2 = T1 2 = (355 K)(2) = 710 K. V1 (c) The maximum pressure is for state 3. For process 2 3, n, R, and T are constant. p2V2 = p3V3 and V p3 = p2 2 = (2.40 105 Pa)(2) = 4.80 105 Pa. V3 (d) process 1 2: W = pV = nRT = (0.250 mol)(8.315 J/mol K)(710 K - 355 K) = 738 K. V 1 process 2 3: W = nRT ln 3 = (0.250 mol)(8.315 J/mol K)(710 K)ln = -1023 J. V2 2 process 3 1: V = 0 and W = 0. The total work done is 738 J + ( -1023 J) = -285 J. This is the work done by the gas. The work done on the gas is 285 J. EVALUATE: The final pressure and volume are the same as the initial pressure and volume, so the final state is the same as the initial state. For the cycle, U = 0 and Q = W = -285 J. During the cycle, 285 J of heat energy must leave the gas. 19.62. Figure 19.62 19.63. IDENTIFY and SET UP: Use the ideal gas law, the first law and expressions for Q and W for specific types of processes. EXECUTE: (a) initial expansion (state 1 state 2) p1 = 2.40 105 Pa, T1 = 355 K, p2 = 2.40 105 Pa, V2 = 2V1 pV = nRT ; T / V = p / nR = constant, so T1 / V1 = T2 / V2 and T2 = T1 (V2 / V1 ) = 355 K(2V1 / V1 ) = 710 K p = 0 so W = pV = nRT = (0.250 mol)(8.3145 J/mol K)(710 K - 355 K) = +738 J Q = nC p T = (0.250 mol)(29.17 J/mol K)(710 K - 355 K) = +2590 J U = Q - W = 2590 J - 738 J = 1850 J 19-18 Chapter 19 (b) At the beginning of the final cooling process (cooling at constant volume), T = 710 K. The gas returns to its original volume and pressure, so also to its original temperature of 355 K. V = 0 so W = 0 Q = nCV T = (0.250 mol)(20.85 J/mol K)(355 K - 710 K) = -1850 J U = Q - W = -1850 J. (c) For any ideal gas process U = nCV T . For an isothermal process T = 0, so U = 0. EVALUATE: The three processes return the gas to its initial state, so U total = 0; our results agree with this. 19.64. IDENTIFY: pV = nRT . For an adiabatic process of an ideal gas, TV1 -1 = T2V2 -1. 1 SET UP: For N 2 , = 1.40. EXECUTE: (a) The pV-diagram is sketched in Figure 19.64. (b) At constant pressure, halving the volume halves the Kelvin temperature, and the temperature at the beginning of the adiabatic expansion is 150 K. The volume doubles during the adiabatic expansion, and from Eq. (19.22), the temperature at the end of the expansion is (150 K)(1 2)0.40 = 114 K. (c) The minimum pressure occurs at the end of the adiabatic expansion (state 3). During the final heating the volume is held constant, so the minimum pressure is proportional to the Kelvin temperature, pmin = (1.80 105 Pa)(114K 300 K) = 6.82 104 Pa. EVALUATE: In the adiabatic expansion the temperature decreases. Figure 19.64 19.65. IDENTIFY: Use the appropriate expressions for Q, W and U for each type of process. U = Q - W can also be used. SET UP: For N 2 , CV = 20.76 J/mol K and C p = 29.07 J/mol K. EXECUTE: (a) W = pV = nRT = (0.150 mol)(8.3145 J mol K)( - 150 K) = -187 J, Q = nC p T = (0.150 mol)(29.07 mol K)( - 150 K) = -654 J, U = Q - W = -467 J. (b) From Eq. (19.24), using the expression for the temperature found in Problem 19.64, 1 W= (0.150 mol)(8.3145 J/mol K)(150 K)(1 - (1/20.40 ) = 113 J. Q = 0 for an adiabatic process, and 0.40 U = Q - W = -W = -113 J. (c) V = 0, so W = 0. Using the temperature change as found in Problem 19.64 and part (b), Q = nCV T = (0.150 mol)(20.76 J mol K)(300 K - 113.7 K) = 580 J and U = Q - W = Q = 580 J. 19.66. EVALUATE: For each process we could also use U = nCV T to calculate U . IDENTIFY: Use the appropriate expression for W for each type of process. SET UP: For a monatomic ideal gas, = 5/ 3 and CV = 3R / 2. EXECUTE: (a) W = nRT ln (V2 / V1 ) = nRT ln (3) = 3.29 103 J. (b) Q = 0 so W = -U = -nCV T . TV1 -1 = T2V2 -1 gives T2 = T1 (1/ 3) 2 / 3 . Then 1 W = nCV T1 (1 - (1 3) 2 / 3 ) = 2.33 103 J. (c) V2 = 3V1 , so W = pV = 2pV1 = 2nRT1 = 6.00 103 J. (d) Each process is shown in Figure 19.66. The most work done is in the isobaric process, as the pressure is maintained at its original value. The least work is done in the adiabatic process. (e) The isobaric process involves the most work and the largest temperature increase, and so requires the most heat. Adiabatic processes involve no heat transfer, and so the magnitude is zero. (f ) The isobaric process doubles the Kelvin temperature, and so has the largest change in internal energy. The isothermal process necessarily involves no change in internal energy. The First Law of Thermodynamics 19-19 EVALUATE: The work done is the area under the path for the process in the pV-diagram. Figure 19.66 shows that the work done is greatest in the isobaric process and least in the adiabatic process. Figure 19.66 19.67. IDENTIFY: Assume the compression is adiabatic. Apply TV1 -1 = T2V2 -1 and pV = nRT . 1 SET UP: For N 2 , = 1.40. V1 = 3.00 L, p = 1.00 atm = 1.013 105 Pa, T = 273.15 K. V2 = V1 / 2 = 1.50 L. -1 V EXECUTE: (a) T2 = T1 1 V2 V = (273.15 K) 1 V1 / 2 0.40 = (273.15 K)(2) 0.4 = 360.4 K = 87.3C. p1V1 p2V2 = . T1 T2 19.68. V T V 360.4 K p2 = p1 1 2 = (1.00 atm) 1 = 2.64 atm. V2 T1 V1 / 2 273.15 K T V nR V V 273.15 K (b) p is constant, so = = constant and 2 = 3 . V3 = V2 3 = (1.50 L) = 1.14 L. T T T2 T3 360.4 K T2 EVALUATE: In an adiabatic compression the temperature increases. IDENTIFY: At equilibrium the net upward force of the gas on the piston equals the weight of the piston. When the piston moves upward the gas expands, the pressure of the gas drops and there is a net downward force on the piston. For simple harmonic motion the net force has the form Fy = - ky, for a displacement y from equilibrium, 1 k . 2 m SET UP: pV = nRT . T is constant. (a) The difference between the pressure, inside and outside the cylinder, multiplied by the area of the piston, must mg mg = p0 + 2 . be the weight of the piston. The pressure in the trapped gas is p0 + A r and f = mg h (b) When the piston is a distance h + y above the cylinder, the pressure in the trapped gas is p0 + 2 r h + y and for values of y small compared to h, h y y = 1 + ~ 1 - . The net force, taking the positive direction to h h+ y h -1 mg y y be upward, is the then Fy = p0 + 2 1 - - p0 ( r 2 ) - mg = - ( p0 r 2 + mg ). r h h This form shows that for positive h, the net force is down; the trapped gas is at a lower pressure than the equilibrium pressure, and so the net force tends to restore the piston to equilibrium. (c) The angular frequency of small oscillations would be given by 2 = ( p r 0 2 + mg ) h m = g p0 r 2 1 + . h mg f = 1 = 2 2 g p0 r 2 1 + . h mg 1/ 2 19-20 Chapter 19 If the displacements are not small, the motion is not simple harmonic. This can be seen be considering what happens if y ~ -h; the gas is compressed to a very small volume, and the force due to the pressure of the gas would become unboundedly large for a finite displacement, which is not characteristic of simple harmonic motion. If y >> h (but not so large that the piston leaves the cylinder), the force due to the pressure of the gas becomes small, and the restoring force due to the atmosphere and the weight would tend toward a constant, and this is not characteristic of simple harmonic motion. h was replaced by 1 - y / h; this is EVALUATE: The assumption of small oscillations was made when h+ y accurate only when y / h is small. 19.69. IDENTIFY: SET UP: W = V2 V1 pdV . For an isothermal process of an ideal gas, W = nRT ln (V2 V1 ) . When a = b = 0, W = nRT ln (V2 V1 ) , as expected. (b) (i) Using the expression found in part (a), W = (1.80 mol )( 8.3145 J/mol K )( 300 K ) EXECUTE: (a) Solving for p as a function of V and T and integrating with respect to V, V2 V - nb nRT an 2 1 2 1 p= - 2 and W = pdV = nRT ln 2 + an - . V1 V - nb V V1 - nb V2 V1 ( 4.00 10 -3 m 3 ) - (1.80 mol ) ( 6.38 10 -5 m 2 / mol ) ln -3 3 -5 2 ( 2.00 10 m ) - (1.80 mol ) ( 6.38 10 m / mol ) 1 1 2 + ( 0.554 J m3 mol2 ) (1.80 mol ) - 4.00 10 -3 m 3 2.00 10-3 m 3 W = 2.80 103 J. (ii) W = nRT ln(2) = 3.11 103 J. (c) The work for the ideal gas is larger by about 300 J. For this case, the difference due to nonzero a is more than that due to nonzero b. The presence of a nonzero a indicates that the molecules are attracted to each other and so do not do as much work in the expansion. EVALUATE: The difference in the two results for W is about 10%, which can be considered to be important.
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UCLA - MAE - 162D
THE SECOND LAW OF THERMODYNAMICS2020.1.IDENTIFY: SET UP:For a heat engine, W = QH - QC . e =W . QH &gt; 0, QC &lt; 0. QHW = 2200 J. QC = 4300 J.EXECUTE: (a) QH = W + QC = 6500 J.2200 J = 0.34 = 34%. 6500 J EVALUATE: Since the engine operates on a cycle,
UCLA - MAE - 162D
ELECTRIC CHARGE AND ELECTRIC FIELD2121.1.(a) IDENTIFY and SET UP: Use the charge of one electron ( -1.602 10-19 C) to find the number of electrons required to produce the net charge. EXECUTE: The number of excess electrons needed to produce net charge
UCLA - MAE - 162D
GAUSS'S LAW22^ E = E cos dA, where is the angle between the normal to the sheet n and the22.1.(a) IDENTIFY and SET UP:electric field E . EXECUTE: In this problem E and cos are constant over the surface so (b) EVALUATE: E = E cos dA = E cos A = (14 N
UCLA - MAE - 162D
ELECTRIC POTENTIAL23ra = 0.150 m rb = (0.250 m) 2 + (0.250 m) 2 rb = 0.3536 m23.1.IDENTIFY: Apply Eq.(23.2) to calculate the work. The electric potential energy of a pair of point charges is given by Eq.(23.9). SET UP: Let the initial position of q2 b
UCLA - MAE - 162D
CAPACITANCE AND DIELECTRICS2424.1.24.2.24.3.Q Vab SET UP: 1 F = 10 -6 F EXECUTE: Q = CVab = (7.28 10-6 F)(25.0 V) = 1.82 10-4 C = 182 C EVALUATE: One plate has charge +Q and the other has charge -Q . PA Q IDENTIFY and SET UP: C = 0 , C = and V = Ed .
UCLA - MAE - 162D
CURRENT, RESISTANCE, AND ELECTROMOTIVE FORCE2525.1.25.2.IDENTIFY: I = Q / t . SET UP: 1.0 h = 3600 s EXECUTE: Q = It = (3.6 A)(3.0)(3600 s) = 3.89 104 C. EVALUATE: Compared to typical charges of objects in electrostatics, this is a huge amount of char
UCLA - MAE - 162D
DIRECT-CURRENT CIRCUITS26 26.1.26.2.26.3.IDENTIFY: The newly-formed wire is a combination of series and parallel resistors. SET UP: Each of the three linear segments has resistance R/3. The circle is two R/6 resistors in parallel. EXECUTE: The resis
UCLA - MAE - 162D
MAGNETIC FIELD AND MAGNETIC FORCES2727.1.IDENTIFY and SET UP: Apply Eq.(27.2) to calculate F . Use the cross products of unit vectors from Section 1.10. ^ j EXECUTE: v = ( +4.19 10 4 m/s ) i + ( -3.85 10 4 m/s ) ^^ (a) B = (1.40 T ) i ^ ^ F = qv B = (
UCLA - MAE - 162D
SOURCES OF MAGNETIC FIELD2828.1.IDENTIFY and SET UP: Use Eq.(28.2) to calculate B at each point. ^ qv r 0 qv r r ^ = B= 0 , since r = . 4 r 2 4 r 3 r 6 ^ and r is the vector from the charge to the point where the field is calculated. v = ( 8.00 10 m/s
UCLA - MAE - 162D
ELECTROMAGNETIC INDUCTION2929.1.29.2.IDENTIFY: Altering the orientation of a coil relative to a magnetic field changes the magnetic flux through the coil. This change then induces an emf in the coil. SET UP: The flux through a coil of N turns is = NBA
UCLA - MAE - 162D
INDUCTANCE30E1 = M30.1.IDENTIFY and SET UP: Apply Eq.(30.4). di EXECUTE: (a) E2 = M 1 = (3.25 10 -4 H)(830 A/s) = 0.270 V; yes, it is constant. dtdi2 ; M is a property of the pair of coils so is the same as in part (a). Thus E1 = 0.270 V. dt EVALUATE
UCLA - MAE - 162D
ALTERNATING CURRENT3131.1.IDENTIFY:i = I cos t and I rms = I/ 2.SET UP: The specified value is the root-mean-square current; I rms = 0.34 A. EXECUTE: (a) I rms = 0.34 A (b) I = 2 I rms = 2(0.34 A) = 0.48 A. (c) Since the current is positive half of t
UCLA - MAE - 162D
ELECTROMAGNETIC WAVES3232.1.IDENTIFY: Since the speed is constant, distance x = ct. SET UP: The speed of light is c = 3.00 108 m/s . 1 yr = 3.156 107 s.32.2.x 3.84 108 m = = 1.28 s c 3.00 108 m/s (b) x = ct = (3.00 108 m/s)(8.61 yr)(3.156 107 s/yr) =
UCLA - MAE - 162D
THE NATURE AND PROPAGATION OF LIGHT3333.1.IDENTIFY: For reflection, r = a . SET UP: The desired path of the ray is sketched in Figure 33.1. 14.0 cm , so = 50.6 . r = 90 - = 39.4 and r = a = 39.4 . EXECUTE: tan = 11.5 cm EVALUATE: The angle of incidence
UCLA - MAE - 162D
GEOMETRIC OPTICS34y = 4.85 cm34.1.IDENTIFY and SET UP: Plane mirror: s = - s (Eq.34.1) and m = y / y = - s / s = +1 (Eq.34.2). We are given s and y and are asked to find s and y. EXECUTE: The object and image are shown in Figure 34.1. s = - s = -39.2
UCLA - MAE - 162D
INTERFERENCE3535.1.35.2.IDENTIFY: Compare the path difference to the wavelength. SET UP: The separation between sources is 5.00 m, so for points between the sources the largest possible path difference is 5.00 m. EXECUTE: (a) For constructive interfer
UCLA - MAE - 162D
DIFFRACTION3636.1.IDENTIFY: Use y = x tan to calculate the angular position of the first minimum. The minima are located by m , m = 1, 2,. First minimum means m = 1 and sin 1 = / a and = a sin 1. Use this Eq.(36.2): sin = a equation to calculate . SET
UCLA - MAE - 162D
RELATIVITY37Figure 37.137.1.IDENTIFY and SET UP: Consider the distance A to O and B to O as observed by an observer on the ground (Figure 37.1).(b) d = vt = (0.900) (3.00 108 m s) (5.05 10-6 s) = 1.36 103 m = 1.36 km. 37.3.1 IDENTIFY and SET UP: The
UCLA - MAE - 162D
PHOTONS, ELECTRONS, AND ATOMS38h f - . The e e38.1.IDENTIFY and SET UP: The stopping potential V0 is related to the frequency of the light by V0 = slope of V0 versus f is h/e. The value fth of f when V0 = 0 is related to by = hf th .EXECUTE: (a) From
UCLA - MAE - 162D
THE WAVE NATURE OF PARTICLES39hc39.1.IDENTIFY and SET UP: EXECUTE: (a) ==h h = . For an electron, m = 9.11 10 -31 kg . For a proton, m = 1.67 10 -27 kg . p mv6.63 10-34 J s = 1.55 10-10 m = 0.155 nm (9.11 10-31 kg)(4.70 106 m/s)m 9.11 10 -31 kg 1
UCLA - MAE - 162D
QUANTUM MECHANICS40n2h 2 . 8mL240.1.IDENTIFY and SET UP: The energy levels for a particle in a box are given by En = EXECUTE: (a) The lowest level is for n = 1, and E1 =(1)(6.626 10-34 J s) 2 = 1.2 10-67 J. 8(0.20 kg)(1.5 m) 21 2E 2(1.2 10-67 J) (b)
UCLA - MAE - 162D
ATOMIC STRUCTURE41L = l (l + 1) . Lz = ml . l = 0, 1, 2,., n - 1. ml = 0, 1, 2,., l . cos = Lz / L .41.1.IDENTIFY and SET UP:EXECUTE: (a) l = 0 : L = 0 , Lz = 0 . l = 1: L = 2 , Lz = ,0, - . l = 2 : L = 6 , Lz = 2 , ,0, - , -2 . (b) In each case cos
UCLA - MAE - 162D
MOLECULES AND CONDENSED MATTER4242.1.3 2 K 2(7.9 10-4 eV)(1.60 10-19 J eV) (a) K = kT T = = = 6.1 K 2 3k 3(1.38 10-23 J K) 2(4.48 eV) (1.60 10 -19 J eV) (b) T = = 34,600 K. 3(1.38 10-23 J K)(c) The thermal energy associated with room temperature (300
UCLA - MAE - 162D
NUCLEAR PHYSICS4343.1.(a) (b) (c)28 14 85 37Si has 14 protons and 14 neutrons. Rb has 37 protons and 48 neutrons. Tl has 81 protons and 124 neutrons.205 8143.2.(a) Using R = (1.2 fm)A1 3 , the radii are roughly 3.6 fm, 5.3 fm, and 7.1 fm. (b) Usin
SUNY Stony Brook - BUS - 220
BUS 220 Introduction to Decision ScienceSpring 2012Assignment 3 due on Thursday, 3/29, 2012NOTE: The assignment could be done jointly by (at most) 2 students. (Of course, it can bedone by a single person.) In any case, the cover page indicating only s
Columbia - IEOR - 4703
IEOR 4703: Homework 5This assignment will help you understand how variance reduction works in real applications. For our first problem: You will estimate the price of a European call option, even though we know the price exactly via Black-Scholes option
Columbia - IEOR - 4703
IEOR 4703: Homework 51. SOLUTION: %Naive Monte Carlo method for K=34, N=300 clear all K=34; S0=35; r=0.05; sigma=0.04; mu=r-sigma^2/2; T=4; N=300; B=randn(1,N); X=mu*T*ones(1,N)+sqrt(T)*sigma*B; S=S0*exp(X); payoff=max(0,S-K*ones(1,N); X_bar=mean(payoff)
Columbia - IEOR - 4703
IEOR 4703: Homework 6Refer to the Lecture Notes 8 (Importance Sampling) (and Class Lecture 7) for the basics needed for this assignment. (Only Problems 3(c)(d) requires programming/simulating.) 1. Consider the random walk Rk = 1 + +k , R0 = 0, in which t
Columbia - IEOR - 4703
IEOR 4703: Solutions to Homework 6Refer to the Lecture Notes 8 (Importance Sampling) (and Class Lecture 7) for the basics needed for this assignment. (Only Problems 3(c)(d) requires programming/simulating.) 1. Consider the random walk Rk = 1 + +k , R0 =
Columbia - IEOR - 4703
IEOR 4703: Homework 71. Consider the problem of estimating(x) = E[eZIcfw_Zx ] Zfor x 1 and where Z N(0, 1). Let X := eIcfw_Zx .(a) Show that (x) (1 - (x)e x where (.) is the CDF of a standard normal random variable. (b) Show that E[X 2 ] (1 - (x)e
Columbia - IEOR - 4703
IEOR 4703: Solutions to Homework 71. Consider the problem of estimating(x) = E[eZIcfw_Zx ] Zfor x 1 and where Z N(0, 1). Let X := eIcfw_Zx .(a) Show that (x) (1 - (x)e x where (.) is the CDF of a standard normal random variable. SOLUTION: Observe
Columbia - IEOR - 4703
IEOR 4703: Homework 8Given a stochastic differential equation (SDE) for a diffusion, dX(t) = a(X(t)dt + b(X(t)dB(t), X(0) = X0 , where cfw_B(t) : t 0 denotes a standard BM, the Euler method for approximating the sample paths of X = cfw_X(t) : 0 t T is g
Columbia - IEOR - 4703
IEOR 4703: Solutions to Homework 81. SOLUTION: clear all close all r=0.05; sigma=0.04; mu=r-sigma^2/2; S0=35; t=4; %Exact Simulation (for your reference) M=10000; X=mu+sigma*randn(t,M); X=tril(ones(t,t)*X; S1=S0*exp(X); Y1=exp(-r*t)*max(0,mean(S1)-40); o
Columbia - IEOR - 4703
IEOR 4703: Homework 91. Gibbs sampler for a closed Jackson queueing network: (READ LECTURE NOTES 10 FOR REFERENCE HERE; SECTION 2.2) Consider a closed queueing network with c = 10 nodes (single-server FIFO queues), and M = 50 customers, in which the 10 1
Columbia - IEOR - 4703
IEOR 4703: Solutions to Homework 9rho=1/10*(1:9); M=50; x=5*ones(1,9); n=10000 N=zeros(9,n); N(:,1)=x; for k=1:n-1 N(:,k+1)=N(:,k); i=ceil(rand*9); B=M-sum(N(:,k)+N(i,k); y=floor(log(rand)/log(rho(i); while (y&gt;B) y=floor(log(rand)/log(rho(i); end N(i,k+1
Columbia - IEOR - 4703
IEOR 4701: Solutions to review of probability problems1. (a) f (x) =xe-x , if x 0; 0, if x &lt; 0.F (x) =0 -x dx 0 xef (y)dy = 1 - e-x , x 0E(X) = = 1/ via integration by parts (U = x, dV = e-x dx). Via integrating the tail, P (X &gt; x) = 1 - F (x) = e-
Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Georgia Tech - CHEM - 2311
IR Spectroscopy Details of Interest1. Alkanesa. Pretty boring landscape throughoutb. Sharp C-H stretch just below 3000 down to around 2850 or soc. Notable C-H scissoring at 1470 and methyl rock 13832. Alkenesa. =C-H Stretch 3100-3000 (not necessaril
Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
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Columbia - IEOR - 4703
IEOR E4703: Practice Midterm Exam, Fall 2010. Professor Sigman. 1. X1 and X2 are two independent random variables distributed as: P (X1 = 0) = 0.30, P (X1 = 1) = 0.50, P (X1 = 2) = 0.20 and P (X2 = 1) = 0.40, P (X2 = 3) = 0.60 (a) Give an algorithm for ge
Columbia - IEOR - 4703
IEOR E4703: Practice Midterm Exam With Solutions, Fall 2010. Professor Sigman. 1. X1 and X2 are two independent random variables distributed as: P (X1 = 0) = 0.30, P (X1 = 1) = 0.50, P (X1 = 2) = 0.20 and P (X2 = 1) = 0.40, P (X2 = 3) = 0.60 (a) Give an a
Columbia - IEOR - 4703
Copyright c 2010 by Karl Sigman1Coupling from the past for Markov chainsGiven a discrete-time Markov chain (MC) cfw_Xn : n 0, with state space S (assumed here to be discrete), and transition matrix P = (Pij ) that is known to have a unique stationary (
Columbia - IEOR - 4703
Copyright c 2010 by Karl Sigman1Rare event simulation and importance samplingSuppose we wish to use Monte Carlo simulation to estimate a probability p = P (A) when the event A is &quot;rare&quot; (e.g., when p is very small). An example would be p = P (Mk &gt; b) w
Columbia - IEOR - 4703
Copyright c 2010 by Karl Sigman1Rare event simulation and importance samplingSuppose we wish to use Monte Carlo simulation to estimate a probability p = P (A) when the event A is &quot;rare&quot; (e.g., when p is very small). An example would be p = P (Mk &gt; b) w
Columbia - IEOR - 4703
Copyright c 2010 by Karl Sigman1Markov Chain Monte Carlo Methods (MCMC)There are many applications in which it is desirable to simulate from a probability distribution (say) in which all specifics of the distribution (cdf, density, etc.) are not known
Columbia - IEOR - 4703
Copyright c 2007 by Karl Sigman1Estimating sensitivitiesWhen estimating the Greeks, such as the , the general problem involves a random variable Y = Y () (such as a discounted payoff) that depends on a parameter of interest (such as initial def price S
Columbia - IEOR - 4706
Columbia University Instructor: Rama CONT Assignment 1. Bond pricing. Assignments should be done individually.M.S. in Financial Engineering Summer 2011.IEOR 4706: Foundations of Financial EngineeringThe table below shows the term structure of (annually
Columbia - IEOR - 4706
Columbia UniversityIEOR 4706: Foundations of Financial EngineeringM.S. in Financial Engineering Summer 2011.Instructor: Rama CONT TA: Jinbeom Kim Assignment 1. Bond pricing.Assignments should be done individually. The table below shows the term struct
Columbia - IEOR - 4706
Columbia - IEOR - 4706
Columbia University Instructor: Rama CONTM.S. in Financial Engineering Summer 2011.IEOR 4706: Foundations of Financial EngineeringSolution for Assignment 3. Arbitrage relations. Part I: Consider an arbitrage-free market in which investors can trade in
Columbia - IEOR - 4706
Columbia - IEOR - 4706
Columbia - IEOR - 4500
IEOR 4500 Introduction to Portfolio OptimizationReferences: The classical reference is Portfolio Selection: Efficient Diversification of Investments, by Harry Markowitz. A more modern reference is: Modern Portfolio Theory and Investment Analysis, by Elto