{"id":1658,"date":"2021-07-19T14:23:07","date_gmt":"2021-07-19T18:23:07","guid":{"rendered":"https:\/\/pressbooks.bccampus.ca\/thermo1\/chapter\/5-1-enthalpy\/"},"modified":"2022-08-10T18:23:55","modified_gmt":"2022-08-10T22:23:55","slug":"5-1-enthalpy","status":"publish","type":"chapter","link":"https:\/\/pressbooks.bccampus.ca\/thermo1\/chapter\/5-1-enthalpy\/","title":{"raw":"5.1 Enthalpy","rendered":"5.1 Enthalpy"},"content":{"raw":"
\r\n

[pb_glossary id=\"811\"]Enthalpy[\/pb_glossary] is an important thermodynamic property for the analysis of energy conservation in open systems. It combines the internal energy and flow work associated with the flowing fluid (see Section 2.2.5<\/a> for details). The following sections explain how to determine the [pb_glossary id=\"1133\"]specific enthalpy[\/pb_glossary] at a given state.<\/p>\r\n\r\n

5.1.1 Using thermodynamic tables to determine specific enthalpy h<\/em><\/h2>\r\n

As described in Chapter 2, thermodynamic tables can be used to determine thermodynamic properties, such as pressure, temperature, specific volume, specific internal energy, specific enthalpy, and specific entropy of a pure substance at a given condition. After the specific enthalpy is found, the enthalpy can then be calculated by using the following equation:<\/p>\r\n\r\n<\/div>\r\n

[latex] H = mh [\/latex]<\/p>\r\n\r\n

\r\n

where<\/p>\r\n

[latex] H [\/latex]: enthalpy, in kJ or J<\/p>\r\n

[latex] h [\/latex]: specific enthalpy, in kJ\/kg or J\/kg<\/p>\r\n

[latex] m [\/latex]: mass of the system, in kg<\/p>\r\n \r\n\r\n<\/div>\r\n

\r\n

Example 1<\/p>\r\n\r\n<\/header> \r\n

Find the missing properties of R134a and ammonia at the given conditions.<\/p>\r\n\r\n

\r\n\r\n\r\n\r\n\r\n\r\n
<\/td>\r\nSubstance<\/td>\r\nT<\/em>, o<\/sup>C<\/strong><\/td>\r\nP<\/em>, kPa<\/strong><\/td>\r\nh<\/em>, kJ\/kg<\/strong><\/td>\r\nx<\/em><\/strong><\/td>\r\nPhase<\/strong><\/td>\r\n<\/tr>\r\n
1<\/td>\r\nR134a<\/td>\r\n20<\/td>\r\n<\/td>\r\n380<\/td>\r\n<\/td>\r\n<\/td>\r\n<\/tr>\r\n
2<\/td>\r\nAmmonia<\/td>\r\n-20<\/td>\r\n200<\/td>\r\n<\/td>\r\n<\/td>\r\n<\/td>\r\n<\/tr>\r\n<\/tbody>\r\n<\/table>\r\nSolution<\/em><\/span>\r\n\r\n1. R134a at T <\/em>= 20o<\/sup>C\u00a0 has a specific enthalpy of h <\/em>= 380 kJ\/kg\r\n
From Appendix C, Table C1<\/a>, at T <\/em>= 20o<\/sup>C, hf <\/sub><\/em>= 227.47 kJ\/kg, hg <\/sub><\/em>= 409.75 kJ\/kg. Since hf <\/sub>< h < hg <\/sub><\/em>, R134a at this state is a two-phase mixture of saturated liquid and saturated vapour with a pressure of P<\/em> = Psat<\/sub><\/em> = 0.57171 MPa = 571.71 kPa and a quality of<\/div>\r\n
<\/div>\r\n
[latex]x=\\displaystyle\\frac{h-h_f}{h_g-h_f} =\\displaystyle\\frac{380-227.47}{409.75-227.47}=0.83679[\/latex]<\/div>\r\n \r\n

2. Ammonia at a temperature of T <\/em>= -20o<\/sup>C and a pressure of P<\/em> = 200 kPa<\/p>\r\n\r\n

From Appendix B, Table B1<\/a>, at T <\/em>= -20o<\/sup>C, Psat<\/sub><\/em> = 0.19008 MPa = 190.08 kPa. Since P<\/em> > Psat<\/sub>, <\/em>ammonia at this state is a compressed liquid with h \u2248 hf<\/sub> = <\/em>251.71 kJ\/kg.<\/div>\r\nIn summary,\r\n\r\n\r\n\r\n\r\n\r\n
<\/td>\r\nSubstance<\/td>\r\nT<\/em>, o<\/sup>C<\/strong><\/td>\r\nP<\/em>, kPa<\/strong><\/td>\r\nh<\/em>, kJ\/kg<\/strong><\/td>\r\nx<\/em><\/strong><\/td>\r\nPhase<\/strong><\/td>\r\n<\/tr>\r\n
1<\/td>\r\nR134a<\/td>\r\n20<\/td>\r\n571.71<\/span><\/td>\r\n380<\/td>\r\n0.83679<\/span><\/td>\r\nTwo-phase mixture<\/span><\/td>\r\n<\/tr>\r\n
2<\/td>\r\nAmmonia<\/td>\r\n-20<\/td>\r\n200<\/td>\r\n251.71<\/span><\/td>\r\nn.a.<\/span><\/td>\r\nCompressed liquid<\/span><\/td>\r\n<\/tr>\r\n<\/tbody>\r\n<\/table>\r\n<\/div>\r\n<\/div>\r\n
\r\n

5.1.2 Constant-pressure specific heat<\/h2>\r\n

[pb_glossary id=\"2624\"]Constant-pressure specific heat[\/pb_glossary] is defined as the energy required to raise the temperature of a unit mass (i.e., 1 kg) of a substance by 1 degree (i.e., 1o<\/sup>C, or 1 K) in an isobaric process. Mathematically, it is expressed as<\/p>\r\n\r\n<\/div>\r\n

[latex]C_p=\\left(\\displaystyle\\frac{\\partial\\ h}{\\partial\\ T}\\right)_p[\/latex]<\/p>\r\n\r\n

\r\n

where<\/p>\r\n

[latex] C_{p} [\/latex]: constant-pressure specific heat, in kJ\/kgK<\/p>\r\n

[latex] h [\/latex]: specific enthalpy, in kJ\/kg<\/p>\r\n

[latex] T [\/latex]: temperature, in K or o<\/sup>C<\/p>\r\n \r\n

The constant-pressure specific heat of selected substances can be found in Appendix G.<\/a> For example, the constant-pressure specific heat of air at 300 K is 1.005 kJ\/kgK, see Table G1<\/a>. Let us consider one kilogram of air originally at 300 K in a piston-cylinder device. It will require 1.005 kJ of heat for the air temperature to increase from 300 K to 301 K if the piston-cylinder device is heated to allow the air to expand in an isobaric process.<\/p>\r\n \r\n

It is important to note that both specific heats, [latex] C_{v} [\/latex] and [latex] C_{p} [\/latex], are properties of a substance. Although they are typically measured in isochoric and isobaric processes, respectively, their applications are NOT limited to isochoric or isobaric processes. For ideal gases, [latex] C_{v} [\/latex] and [latex] C_{p} [\/latex] can be used to determine [latex] \\Delta u [\/latex] and [latex] \\Delta h [\/latex], respectively, in ANY<\/strong> processes.<\/p>\r\n\r\n

5.1.3 Using C<\/em>p<\/em><\/sub> to calculate \u0394h<\/em> for ideal gases<\/h2>\r\nThe specific enthalpy of an ideal gas is a function of temperature only, [latex]h = f(T)[\/latex]; therefore,\r\n

[latex]C_p=\\left(\\displaystyle\\frac{\\partial\\ h}{\\partial\\ T}\\right)_p = \\left(\\dfrac{dh}{dT}\\right)_p=f(T)[\/latex]<\/p>\r\n \r\n\r\nThe change of specific enthalpy of an ideal gas within a small temperature range can be calculated as\r\n

[latex]\\Delta h = h_2-h_1 = C_p(T_2-T_1)[\/latex]<\/p>\r\nwhere\r\n

[latex] C_{p} [\/latex]: constant-pressure specific heat in a small temperature range, in kJ\/kgK<\/p>\r\n

[latex] h [\/latex]: specific enthalpy, in kJ\/kg<\/p>\r\n

[latex] T [\/latex]: temperature, in K or o<\/sup>C<\/p>\r\n

Subscripts 1 and 2 represent states 1 and 2 in a process, respectively.<\/p>\r\n \r\n\r\nThe above formula is a simple, approximate method to estimate the change of specific enthalpy of an ideal gas due to temperature variations. It is reasonably accurate and may be used when the thermodynamic tables of an ideal gas are not available. Table G1<\/a> lists the constant-pressure specific heat of selected substances at 300 K. Strictly speaking, since [latex] C_{p}=f(T) [\/latex], [latex] C_{p}[\/latex] at a different temperature should be calculated according to that specific temperature. However, <\/span>Table G1<\/a> is often used in approximate calculations as long as the temperature variations of the ideal gas remain in a small range. <\/span>\r\n\r\n \r\n\r\nThe specific heat ratio, [latex]k[\/latex], of an ideal gas is defined as the ratio of [latex] C_{p} [\/latex] to [latex] C_{v} [\/latex].\r\n\r\n \r\n

[latex]k=\\displaystyle\\frac{C_p}{C_v}[\/latex]<\/p>\r\n \r\n

The <\/span>following equations relate [latex] C_{v} [\/latex], [latex] C_{p} [\/latex], [latex] k [\/latex], <\/span>and [latex] R [\/latex]. Detailed derivations are omitted here.<\/p>\r\n

[latex]C_p=C_v+R[\/latex]\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 [latex]C_p=\\displaystyle\\frac{kR}{k-1}[\/latex]\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 [latex]C_v=\\displaystyle\\frac{R}{k-1}[\/latex]<\/p>\r\n\r\n

5.1.4 Using C<\/em>p<\/em><\/sub> to calculate \u0394h<\/em> for solids and liquids<\/h2>\r\nLiquids and solids are generally treated as incompressible substances because their volumes do not change with pressure or temperature significantly. For liquids and solids, the difference between the constant-volume specific heat and the constant-pressure specific heat is typically negligible; t<\/span>herefore,<\/span>\r\n\r\n \r\n

[latex]C_p \\approx C_v[\/latex]<\/p>\r\n \r\n

[latex]\\Delta h \\approx\\ \\Delta u\\approx\\ C_p(T_2-T_1)[\/latex]<\/p>\r\n \r\n

\r\n

Example 2<\/p>\r\n\r\n<\/header>\r\n

\r\n

Consider a piston-cylinder device containing 2 kg of oxygen at 300 K, 200 kPa. The piston-cylinder device is made of 0.5 kg of aluminum. How much heat is required for the oxygen to reach a temperature of 600 K in an isobaric process? Assume the oxygen and the piston-cylinder are always in thermal equilibrium during the isobaric process. The oxygen can be treated as an ideal gas in this heating process.<\/p>\r\n \r\n

Solution<\/em><\/span><\/p>\r\n

First, set up a closed system as shown outlined in blue, which consists of the piston-cylinder and O<\/span>2.\u00a0<\/sub><\/p>\r\n \r\n\r\n[caption id=\"attachment_2304\" align=\"aligncenter\" width=\"226\"]\"Piston-cylinder<\/a> Figure 5.1.e1<\/strong> Piston-cylinder device containing oxygen<\/em>[\/caption]\r\n

Second, apply the first law of thermodynamics to the closed system. Note that, in the heating process, the temperatures and internal energies of both O2<\/sub> and the piston-cylinder increase.\r\n<\/span><\/p>\r\n

[latex]\\because \\Delta U_{tot} = Q_{tot} - W_{O_{2}} [\/latex]\u00a0\u00a0 and\u00a0\u00a0 [latex]\\Delta U_{tot} = \\Delta U_{O_{2}} + \\Delta U_{al} [\/latex]\r\n<\/span><\/p>\r\n

[latex]\\therefore Q_{tot} = \\Delta U_{tot} + W_{O_{2}} = \\Delta U_{al} + (\\Delta U_{O_{2}} + W_{O_{2}}) [\/latex]<\/span><\/p>\r\n \r\n\r\nThird, calculate the change in internal energy of the piston-cylinder. From Table G3<\/a>, the constant-pressure specific heat for aluminum is [latex]C_{p,al}[\/latex]= 0.897 kJ\/kgK.\r\n

[latex]\\begin{align*} \\Delta U_{al} &= m_{al}\\Delta u_{al} = m_{al}\\Delta h_{al} \\\\&= m_{al}C_{p,al}(T_2 - T_1) \\\\&= 0.5 \\times 0.897 \\times (600-300)= 134.55 \\ \\rm{kJ}\\end{align*}[\/latex]<\/p>\r\n \r\n\r\nFourth, analyze the boundary work done by O2<\/sub> and the change in internal energy of O2<\/sub> in this isobaric process, where [latex]P_1=P_2=P[\/latex].\r\n

[latex]\\begin{align*} \\because\u00a0 \\; \\; W_{O_{2}} &= P(\\mathbb{V}_2 - \\mathbb{V}_1) \\; \\; \\; \\; \\Delta U_{O_{2}} = U_2 - U_1\u00a0 \\\\ H &=U+P\\mathbb{V} \\end{align*}[\/latex]<\/p>\r\n

[latex] \\begin{align*} \\therefore \\; \\Delta U_{O_{2}} + W_{O_{2}} &= (U_2 - U_1) + P(\\mathbb{V}_2 - \\mathbb{V}_1) \\\\&= (U_2 + P_2\\mathbb{V}_2) - (U_1 + P_1\\mathbb{V}_1) \\\\&= H_2 - H_1 \\end{align*}[\/latex]<\/p>\r\n

[latex] \\therefore \\Delta U_{O_{2}} + W_{O_{2}} = \\Delta H_{O_{2}} [\/latex] (for isobaric process)<\/p>\r\n

From Table G1<\/a>, the constant-pressure specific heat for oxygen is [latex] C_{p,O_{2}} [\/latex] = 0.918 kJ\/kgK.<\/p>\r\n

[latex] \\begin{align*} \\therefore \\Delta H_{O_{2}} &= m_{O_{2}}C_{p,O_{2}}(T_2 - T_1) \\\\&= 2 \\times 0.918 \\times (600-300) = 550.8 \\ \\rm{kJ} \\end{align*}[\/latex]<\/p>\r\n \r\n\r\nLast, calculate the total heat transfer in this process.\r\n

[latex]\\begin{align*} Q_{tot} &= \\Delta U_{al} + \\Delta H_{O_{2}} \\\\&= 134.55+550.8= 685.35 \\ \\rm{kJ} \\end{align*}[\/latex]<\/p>\r\n

<\/p>\r\n\r\n<\/div>\r\n<\/div>\r\n<\/div>\r\n

\r\n

Practice Problems<\/p>\r\n\r\n<\/header>\r\n

[h5p id=\"36\"]<\/div>\r\n<\/div>","rendered":"
\n

Enthalpy<\/a> is an important thermodynamic property for the analysis of energy conservation in open systems. It combines the internal energy and flow work associated with the flowing fluid (see Section 2.2.5<\/a> for details). The following sections explain how to determine the specific enthalpy<\/a> at a given state.<\/p>\n

5.1.1 Using thermodynamic tables to determine specific enthalpy h<\/em><\/h2>\n

As described in Chapter 2, thermodynamic tables can be used to determine thermodynamic properties, such as pressure, temperature, specific volume, specific internal energy, specific enthalpy, and specific entropy of a pure substance at a given condition. After the specific enthalpy is found, the enthalpy can then be calculated by using the following equation:<\/p>\n<\/div>\n

[latex]H = mh[\/latex]<\/p>\n

\n

where<\/p>\n

[latex]H[\/latex]: enthalpy, in kJ or J<\/p>\n

[latex]h[\/latex]: specific enthalpy, in kJ\/kg or J\/kg<\/p>\n

[latex]m[\/latex]: mass of the system, in kg<\/p>\n

 <\/p>\n<\/div>\n

\n
\n

Example 1<\/p>\n<\/header>\n

 <\/p>\n

Find the missing properties of R134a and ammonia at the given conditions.<\/p>\n

\n\n\n\n\n\n
<\/td>\nSubstance<\/td>\nT<\/em>, o<\/sup>C<\/strong><\/td>\nP<\/em>, kPa<\/strong><\/td>\nh<\/em>, kJ\/kg<\/strong><\/td>\nx<\/em><\/strong><\/td>\nPhase<\/strong><\/td>\n<\/tr>\n
1<\/td>\nR134a<\/td>\n20<\/td>\n<\/td>\n380<\/td>\n<\/td>\n<\/td>\n<\/tr>\n
2<\/td>\nAmmonia<\/td>\n-20<\/td>\n200<\/td>\n<\/td>\n<\/td>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n

Solution<\/em><\/span><\/p>\n

1. R134a at T <\/em>= 20o<\/sup>C\u00a0 has a specific enthalpy of h <\/em>= 380 kJ\/kg<\/p>\n

From Appendix C, Table C1<\/a>, at T <\/em>= 20o<\/sup>C, hf <\/sub><\/em>= 227.47 kJ\/kg, hg <\/sub><\/em>= 409.75 kJ\/kg. Since hf <\/sub>< h < hg <\/sub><\/em>, R134a at this state is a two-phase mixture of saturated liquid and saturated vapour with a pressure of P<\/em> = Psat<\/sub><\/em> = 0.57171 MPa = 571.71 kPa and a quality of<\/div>\n
<\/div>\n
[latex]x=\\displaystyle\\frac{h-h_f}{h_g-h_f} =\\displaystyle\\frac{380-227.47}{409.75-227.47}=0.83679[\/latex]<\/div>\n

 <\/p>\n

2. Ammonia at a temperature of T <\/em>= -20o<\/sup>C and a pressure of P<\/em> = 200 kPa<\/p>\n

From Appendix B, Table B1<\/a>, at T <\/em>= -20o<\/sup>C, Psat<\/sub><\/em> = 0.19008 MPa = 190.08 kPa. Since P<\/em> > Psat<\/sub>, <\/em>ammonia at this state is a compressed liquid with h \u2248 hf<\/sub> = <\/em>251.71 kJ\/kg.<\/div>\n

In summary,<\/p>\n\n\n\n\n\n
<\/td>\nSubstance<\/td>\nT<\/em>, o<\/sup>C<\/strong><\/td>\nP<\/em>, kPa<\/strong><\/td>\nh<\/em>, kJ\/kg<\/strong><\/td>\nx<\/em><\/strong><\/td>\nPhase<\/strong><\/td>\n<\/tr>\n
1<\/td>\nR134a<\/td>\n20<\/td>\n571.71<\/span><\/td>\n380<\/td>\n0.83679<\/span><\/td>\nTwo-phase mixture<\/span><\/td>\n<\/tr>\n
2<\/td>\nAmmonia<\/td>\n-20<\/td>\n200<\/td>\n251.71<\/span><\/td>\nn.a.<\/span><\/td>\nCompressed liquid<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<\/div>\n
\n

5.1.2 Constant-pressure specific heat<\/h2>\n

Constant-pressure specific heat<\/a> is defined as the energy required to raise the temperature of a unit mass (i.e., 1 kg) of a substance by 1 degree (i.e., 1o<\/sup>C, or 1 K) in an isobaric process. Mathematically, it is expressed as<\/p>\n<\/div>\n

[latex]C_p=\\left(\\displaystyle\\frac{\\partial\\ h}{\\partial\\ T}\\right)_p[\/latex]<\/p>\n

\n

where<\/p>\n

[latex]C_{p}[\/latex]: constant-pressure specific heat, in kJ\/kgK<\/p>\n

[latex]h[\/latex]: specific enthalpy, in kJ\/kg<\/p>\n

[latex]T[\/latex]: temperature, in K or o<\/sup>C<\/p>\n

 <\/p>\n

The constant-pressure specific heat of selected substances can be found in Appendix G.<\/a> For example, the constant-pressure specific heat of air at 300 K is 1.005 kJ\/kgK, see Table G1<\/a>. Let us consider one kilogram of air originally at 300 K in a piston-cylinder device. It will require 1.005 kJ of heat for the air temperature to increase from 300 K to 301 K if the piston-cylinder device is heated to allow the air to expand in an isobaric process.<\/p>\n

 <\/p>\n

It is important to note that both specific heats, [latex]C_{v}[\/latex] and [latex]C_{p}[\/latex], are properties of a substance. Although they are typically measured in isochoric and isobaric processes, respectively, their applications are NOT limited to isochoric or isobaric processes. For ideal gases, [latex]C_{v}[\/latex] and [latex]C_{p}[\/latex] can be used to determine [latex]\\Delta u[\/latex] and [latex]\\Delta h[\/latex], respectively, in ANY<\/strong> processes.<\/p>\n

5.1.3 Using C<\/em>p<\/em><\/sub> to calculate \u0394h<\/em> for ideal gases<\/h2>\n

The specific enthalpy of an ideal gas is a function of temperature only, [latex]h = f(T)[\/latex]; therefore,<\/p>\n

[latex]C_p=\\left(\\displaystyle\\frac{\\partial\\ h}{\\partial\\ T}\\right)_p = \\left(\\dfrac{dh}{dT}\\right)_p=f(T)[\/latex]<\/p>\n

 <\/p>\n

The change of specific enthalpy of an ideal gas within a small temperature range can be calculated as<\/p>\n

[latex]\\Delta h = h_2-h_1 = C_p(T_2-T_1)[\/latex]<\/p>\n

where<\/p>\n

[latex]C_{p}[\/latex]: constant-pressure specific heat in a small temperature range, in kJ\/kgK<\/p>\n

[latex]h[\/latex]: specific enthalpy, in kJ\/kg<\/p>\n

[latex]T[\/latex]: temperature, in K or o<\/sup>C<\/p>\n

Subscripts 1 and 2 represent states 1 and 2 in a process, respectively.<\/p>\n

 <\/p>\n

The above formula is a simple, approximate method to estimate the change of specific enthalpy of an ideal gas due to temperature variations. It is reasonably accurate and may be used when the thermodynamic tables of an ideal gas are not available. Table G1<\/a> lists the constant-pressure specific heat of selected substances at 300 K. Strictly speaking, since [latex]C_{p}=f(T)[\/latex], [latex]C_{p}[\/latex] at a different temperature should be calculated according to that specific temperature. However, <\/span>Table G1<\/a> is often used in approximate calculations as long as the temperature variations of the ideal gas remain in a small range. <\/span><\/p>\n

 <\/p>\n

The specific heat ratio, [latex]k[\/latex], of an ideal gas is defined as the ratio of [latex]C_{p}[\/latex] to [latex]C_{v}[\/latex].<\/p>\n

 <\/p>\n

[latex]k=\\displaystyle\\frac{C_p}{C_v}[\/latex]<\/p>\n

 <\/p>\n

The <\/span>following equations relate [latex]C_{v}[\/latex], [latex]C_{p}[\/latex], [latex]k[\/latex], <\/span>and [latex]R[\/latex]. Detailed derivations are omitted here.<\/p>\n

[latex]C_p=C_v+R[\/latex]\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 [latex]C_p=\\displaystyle\\frac{kR}{k-1}[\/latex]\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0\u00a0 [latex]C_v=\\displaystyle\\frac{R}{k-1}[\/latex]<\/p>\n

5.1.4 Using C<\/em>p<\/em><\/sub> to calculate \u0394h<\/em> for solids and liquids<\/h2>\n

Liquids and solids are generally treated as incompressible substances because their volumes do not change with pressure or temperature significantly. For liquids and solids, the difference between the constant-volume specific heat and the constant-pressure specific heat is typically negligible; t<\/span>herefore,<\/span><\/p>\n

 <\/p>\n

[latex]C_p \\approx C_v[\/latex]<\/p>\n

 <\/p>\n

[latex]\\Delta h \\approx\\ \\Delta u\\approx\\ C_p(T_2-T_1)[\/latex]<\/p>\n

 <\/p>\n

\n
\n

Example 2<\/p>\n<\/header>\n

\n

Consider a piston-cylinder device containing 2 kg of oxygen at 300 K, 200 kPa. The piston-cylinder device is made of 0.5 kg of aluminum. How much heat is required for the oxygen to reach a temperature of 600 K in an isobaric process? Assume the oxygen and the piston-cylinder are always in thermal equilibrium during the isobaric process. The oxygen can be treated as an ideal gas in this heating process.<\/p>\n

 <\/p>\n

Solution<\/em><\/span><\/p>\n

First, set up a closed system as shown outlined in blue, which consists of the piston-cylinder and O<\/span>2.\u00a0<\/sub><\/p>\n

 <\/p>\n

\"Piston-cylinder<\/a>
Figure 5.1.e1<\/strong> Piston-cylinder device containing oxygen<\/em><\/figcaption><\/figure>\n

Second, apply the first law of thermodynamics to the closed system. Note that, in the heating process, the temperatures and internal energies of both O2<\/sub> and the piston-cylinder increase.
\n<\/span><\/p>\n

[latex]\\because \\Delta U_{tot} = Q_{tot} - W_{O_{2}}[\/latex]\u00a0\u00a0 and\u00a0\u00a0 [latex]\\Delta U_{tot} = \\Delta U_{O_{2}} + \\Delta U_{al}[\/latex]
\n<\/span><\/p>\n

[latex]\\therefore Q_{tot} = \\Delta U_{tot} + W_{O_{2}} = \\Delta U_{al} + (\\Delta U_{O_{2}} + W_{O_{2}})[\/latex]<\/span><\/p>\n

 <\/p>\n

Third, calculate the change in internal energy of the piston-cylinder. From Table G3<\/a>, the constant-pressure specific heat for aluminum is [latex]C_{p,al}[\/latex]= 0.897 kJ\/kgK.<\/p>\n

[latex]\\begin{align*} \\Delta U_{al} &= m_{al}\\Delta u_{al} = m_{al}\\Delta h_{al} \\\\&= m_{al}C_{p,al}(T_2 - T_1) \\\\&= 0.5 \\times 0.897 \\times (600-300)= 134.55 \\ \\rm{kJ}\\end{align*}[\/latex]<\/p>\n

 <\/p>\n

Fourth, analyze the boundary work done by O2<\/sub> and the change in internal energy of O2<\/sub> in this isobaric process, where [latex]P_1=P_2=P[\/latex].<\/p>\n

[latex]\\begin{align*} \\because\u00a0 \\; \\; W_{O_{2}} &= P(\\mathbb{V}_2 - \\mathbb{V}_1) \\; \\; \\; \\; \\Delta U_{O_{2}} = U_2 - U_1\u00a0 \\\\ H &=U+P\\mathbb{V} \\end{align*}[\/latex]<\/p>\n

[latex]\\begin{align*} \\therefore \\; \\Delta U_{O_{2}} + W_{O_{2}} &= (U_2 - U_1) + P(\\mathbb{V}_2 - \\mathbb{V}_1) \\\\&= (U_2 + P_2\\mathbb{V}_2) - (U_1 + P_1\\mathbb{V}_1) \\\\&= H_2 - H_1 \\end{align*}[\/latex]<\/p>\n

[latex]\\therefore \\Delta U_{O_{2}} + W_{O_{2}} = \\Delta H_{O_{2}}[\/latex] (for isobaric process)<\/p>\n

From Table G1<\/a>, the constant-pressure specific heat for oxygen is [latex]C_{p,O_{2}}[\/latex] = 0.918 kJ\/kgK.<\/p>\n

[latex]\\begin{align*} \\therefore \\Delta H_{O_{2}} &= m_{O_{2}}C_{p,O_{2}}(T_2 - T_1) \\\\&= 2 \\times 0.918 \\times (600-300) = 550.8 \\ \\rm{kJ} \\end{align*}[\/latex]<\/p>\n

 <\/p>\n

Last, calculate the total heat transfer in this process.<\/p>\n

[latex]\\begin{align*} Q_{tot} &= \\Delta U_{al} + \\Delta H_{O_{2}} \\\\&= 134.55+550.8= 685.35 \\ \\rm{kJ} \\end{align*}[\/latex]<\/p>\n

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Practice Problems<\/p>\n<\/header>\n

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