C e. Negative. In a clockwise cycle, the work done on the gas is negative. Or for the cycle Qnet = +600 J and U = 0 so W = Q = 600 J

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AP Physics Free Response Practice Thermodynamics ANSWERS 1983B4 Since T is constant, pbv B = p 0 V 0 and V B = 2V 0 gives p B = ½ p0 U = Q + W, since AB is isothermal, U = 0 and W = Q = 1000 J c. The entropy of the gas increases because S = Q/T and Q is positive (heat was added) d. QH TH In a reversible (Carnot) engine giving Qc = 400 J Q T C C e. Negative. In a clockwise cycle, the work done on the gas is negative. Or for the cycle Qnet = +600 J and U = 0 so W = Q = 600 J 1996B7 p1/t 1 = p 2 /T 2 gives p 2 = 0.82 atm = 8.2 10 4 Pa F = p Area = 410 N c. Since volume and temperature are constant, we can use p 1 V = n 1 RT and p 2 V = n 2 RT. SUbtractnig the two equations gives pv = nrt, or n = pv/rt = 5.45 10 3 mol 1986B5 T H T C ec (use absolute temperature) gives e c = 0.074 TH e = W/QH, or Q H = W/e = (100 MW)/(0.074) = 1350 MW and Q C = Q H W = 1250 MW (note Q may represent heat in Joules or rate in Watts) c. AB is isothermal so T = 0. It is an expansion so W is and Q = W BC is adiabatic so Q = 0. Temperature drops so T is negative. CD is isothermal so T = 0. It is a compression so W is + and Q = W BC is adiabatic so Q = 0. Temperature rises so T is positive. 2004B5B Since PA = P B and V A /T A = V B /T B giving T B = T 2 = T 1 /2 CA is an isotherm so TA = T C so P A V A = P C V C ; P 1 V 1 = P 2 (V 1 /2) giving P 2 = 2P1 c. Work is the area under the line. No work is done from B to C so we just need the area under line AB. Specifically, W = P V = P1(V 1 /2 V 1 ) = +½P 1 V1 d. Heat was added in processes BC and CA, but not in AB. BC: W = 0 so U = Q and temperature rises so U is positive CA: U = 0 (isotherm) so Q = W and it is an expansion so W is negative and therefore Q is positive AB: Compression so W is + and temperature drops so U is negative and Q = U W which must be negative 393

1989B4 i. The work done on the gas is the area enclosed. Area = width height = 2V 0 P 0 = 2P 0 V 0 (negative since it is a clockwise cycle) ii. U = 0 for any cycle iii. since U = 0, Q = W = +2P 0 V0 c. For process 2, W = P V = 2P0 (3V 0 V 0 ) = 4P 0 V 0 and U = 3/2 nr T = 3/2 nr(6t 0 2T 0 ) = +6 nrt 0 = +6P 0 V 0 Q = U W = +6 P 0 V 0 ( 4P 0 V 0 ) = +10P 0 V 0 1999B7 Since TA = T C, P A V A = P C V C giving P C = 2 10 5 Pa c. This is a clockwise cycle so the work done on the gas is negative. d. This is a clockwise cycle so this is a heat engine. 2001B6 The additional pressure comes from the weight of the added block. P = F/A = mg/a = 2.04 10 3 Pa and P 2 = P 1 + P = 1.04 10 5 Pa A constant temperature, P1V 1 = P 2 V 2, or V 2 = P 1 V 1 /P 2 = 1.47 10 3 3 m c. Since the external pressure and the added weight do not change, the pressure remains constant, therefore the process from state 2 to state 3 is isobaric d. For similar reasons as stated above, the process from state 4 to state 1 is also isobaric. e. Comparing state 1 and state 4, which have equal pressures: V 1 /T 1 = V 4 /T 4, giving V 4 = V 1 T 4 /T 1 = 2.05 10 3 m 3 394

2006B5 i. P1 = P 2 so V 1 /T 1 = V 2 /T 2 giving T 2 = 746 K ii. V1 = V 3 so P 1 /T 1 = P 3 /T 3 giving T 3 = 560 K The net work done is the area enclosed by the triangle = ½ base height = +6250 J (positive since the cycle is counterclockwise) c. Since the cycle is counterclockwise, the work done on the gas is positive (more area under the process 2 3 in which positive work is done than in process 1 2 where negative work is done). In any cycle U = 0 so we have Q = W, therefore Q is negative meaning heat is removed. 2003B5 Ua U c = U ca = Q ca + W ca = 685 J + ( 120 J) = 565 J i/ii. Heat is removed. Uabc = U ca = 565 J since it is the opposite beginning and end points, the path doesn t matter. Q = U W = 565 J 75 J = 640 J c. Wcda = W cd + W da = 0 + P V da = 150 J d. Heat is added. U = +565 J and W = 150 J and Q = U W 2003B5B 3 pv = nrt so T = pv/nr = (200 Pa)(20 m )/(1 mol)(8.32 J/(mol-K)) = 481 K The net work done is the area enclosed by the triangle = ½ base height = +4000 J (positive since the cycle is counterclockwise) c. i/ii. Heat is removed. In one cycle U = 0 so Q = W = 4000 J d. In a cyclic process U = 0 (the temperature returns to the same value) e. The entropy is a function of the state of the gas, and after one complete cycle the gas has returned to its original state so the entropy is the same. 2004B5 i. W = P V = 3600 J. The work done by the gas is the negative of the work done on the gas, +3600 J ii. U = 3/2 nr T and the temperatures can be found from PV = nrt giving T A = 108 K and T B = 325 K so U = 5400 J iii. U = Q + W so Q = U W = +9000 J (remember, the W in this equation is the work done on the gas) c. ii. Heat is removed. In an isothermal process, U = 0 so Q = W and in a compression W is positive. 395

2008B5 Since process AB is isochoric, V = 0 therefore W = P V = 0 (also, there is no area under the line) At constant volume for a fixed number of moles, pressure is directly related to temperature and since the pressure increases, so does the temperature. U is directly related to T so it is positive. Q = U W and W = 0 c. Since T B = T C, P B V B = P C V C so V C = P B V B /P C = 0.005 m 3 2005B6 The volume of the cylinder = Area height = AH. PV = nrt then becomes PAH = nrt so H = nrt/pa c. Calculating the slope of the line above and setting it equal to the slope from the equation of part a: nr/pa gives n = 1.11 moles 2005B6B PV = nrt or P = (1/V)nRT The total pressure is the atmospheric pressure plus the pressure due to the added mass P = P atm + mg/a c. d. From P = (1/V)nRT, the slope of the above line = nrt. Slope = 6.19 Pa-m 3 so n =.0025 moles 396

2006B5B i. TA = T B so P A V A = P B V B : P B /P A = ½ ii. PB = P C so P C /P A = P B /P A = ½ iii. A and B are on the same isotherm so T B/T A = 1 iv. VC = V A so P C /P A = T C /T A = ½ Internal energy depends only on the temperature. Since step I is isothermal there is no change in temperature and thus no change in internal energy c. W = P V. In step III there is no change in volume, and thus no work done. 2007B5 P = F/A so F = PA = P( R 2 ) = (4.0 10 5 Pa) (½ 0.20 m) 2 = 1.3 10 4 N PV = nrt gives V = 1.2 10 2 3 m c. Won the gas = P V so W by the gas = +P V where V = Ax = R 2 x and x = extra distance pushed by the piston giving W by = 1.9 10 3 J d. Heat is transferred to the gas. This is an expansion so Won is negative. For the gas to expand at constant pressure, the temperature must also increase so U is positive. Q = U W. 2007B5B i. For the piston to be in equilibrium, the gas must hold it up against its own weight and the external force due to the outside pressure: F = PatmA + Mg where A = R 2 = (D/2) 2 = D 2 /4 so we have F = ¼P atm D 2 + Mg ii. P = F/A = F from above ¼ D 2 2 giving P abs = P atm + 4Mg/ D Pressure goes up. If heat is added at constant volume, the temperature goes up and so must the pressure since P T at constant volume. c. W = Fx (from mechanics) = (¼P atm D 2 + Mg)x 0 2008B6B V1 = V 2 so P 1 /T 1 = P 2 /T 2 giving T 2 = 1500 K; P 1 = P 3 so V 1 /T 1 = V 3 /T 3 giving T 3 = 1800 K b/c. The net work done is the area enclosed by the triangle = ½ base height = 100 J (negative since clockwise) d. For process 1 2 W = 0 so Q = U = 3/2 nr T = (1.5)(0.004 mol)(8.31 J/mol-K)(1500 K 300 K) = 60 J 2009B4 PV = nrt so T = PV/nR and the number of moles = (2.2 10 3 g of H 2 O)/(18 g/mole) = 122.2 moles. This gives T = (3 10 5 Pa)(2 m 3 )/(122.2 moles)(8.31 J/mol-K) = 591 K The temperature is proportional to the product of P and V. (PV) A = 6 10 5 J and (PV) C = 10 10 5 J so T C /T A = 10/6 giving T C = 985 K c. Since the temperature increases for process A B C and U is dependent on the temperature, U increases. d. W ABC = W AB + W BC = 0 + P V = (4 10 5 Pa)(2.5 m 3 2 m 3 ) = 2 10 5 J 1974B6 PAV A /T A = P B V B /T B ; (1.5 atm)(1 L)/T A = (0.5 atm)(3 L)/T B giving T A = TB Since TA = T B, U AB = 0. W is the area under the line = 2 L-atm (negative for an expansion) and we have Q = U W = +2 L-atm = +202.6 J c. PV/T is constant so highest temperature is at the highest value of PV where P = 1 atm and V = 2 L. PV = nrt gives T = 243 K 1975B3 The work done on the gas is the area enclosed by the cycle = length width = 4p0V 0 (negative since clockwise) In the cycle U = 0 so Q = W = +4p0V0 c. Temperature is the same where the product p V is the same: A = p0v 0 ; B = 3p 0 V 0 ; C = 9p 0 V 0 ; D = 3p 0 V 0 ; T B = TD d. AB: Q = U W = 3/2 nr T 0 and T = 2T0 ; so Q = +3nRT 0 = +3p 0 V 0 BC: Q = U W = 3/2 nr T ( p V) and T = 6T 0 ; so Q = 9p 0 V 0 ( 6p 0 V 0 ) = +15p 0 V 0 Q BC > Q AB 397

1979B5 Process II is isothermal. An isothermal process is one in which the temperature is constant. Thus, from the ideal gas law, the product of pressure and volume is a constant. This condition is satisfied by process II. Process III is adiabatic. In an adiabatic process, both the pressure and the volume must change. Thus, processes I and IV are eliminated. Since process II is isothermal, process III is the only possible adiabatic one. c. The gas does work in processes I, II and III. Work is done by the gas whenever the volume increases. (negative work is done by the gas when the volume decreases as well) d. In process IV, no work is done. Since the pressure decreases at constant volume, the temperature also decreases, giving U is negative and with W = 0, U = Q and therefore Q is negative. One could also use the adiabatic process as the dividing line between process in which heat is added and those for which heat is removed. On the adiabatic line, Q = 0. For any process from the same initial point that lies above the adiabat, heat is added and for any process that lies below the adiabat, heat is removed. e. RMS speed is proportional to the kinetic energy which, in turn, is proportional to the temperature. Only in process I does the temperature increase. 1991B3 Power is the rate of useful work form an engine so W (which here represents the rate in MW) = 120 MW and e = W/QH = 0.40 = 120 MW/Q H giving Q H = 300 MW The rate of heat input from the combustion of oil is 300 Joules per second. Since oil provides 4.4 10 7 joules per kilogram burned we can divide to find the number of kg per second that must be combusted: m/ t = (300 10 6 J/s) (4.4 10 7 J/kg) = 6.82 kg/s c. QC = Q H W = 180 MW 1993B5 Since Pa = P b, V a /T a = V b /T b giving T b = 750 K b/c. Uab = 3/2 nr T = (1.5)(1 mole)(8.32 J/mol-K)(750 K 250 K) = 6240 J W ab = P V = (1.2 10 5 Pa)(51 10 3 m 3 17 10 3 m 3 ) = 4080 J Q = U W = 10,320 J d. W = P V = 0 (no area under the line) e. In a cycle U = 0 so W = Q = 1800 J T H T C f. ec = 0.66 T H 1995B5 2 P = Fv (from mechanics) = mgv = (10 kg)(10 m/s )(4 m/s) = 400 W T H T C ec = 0.4 or 40% TH c. i. With an efficiency of 0.4 and useful work done at the rate of 400 W we have e = (W/t)/(Q H /t) or (Q H /t) = 1000 W ii. (QC/t) = Q H /t) (W/t) = 600 W 398