Question #122704
0.05kg of CO² with MW=44,occupying a volume of 0.03m³ at 1.025bar,is compressed reversible until the pressure is 6.15bar. Calculate final temperature, the work done on the CO²,the heat flow to or form the cylinder walls
(i)when the process is according to law pV¹.⁴=constant
(ii)when the process is Isothermal
(iii)when the process takes place in a perfectly thermal insulated cylinder.
Assume CO² to be a perfect gas takes Y=1.3
1
Expert's answer
2020-06-18T10:59:25-0400

The mass is m=0.05kg,m = 0.05\,\mathrm{kg}, μ=44g/mol\mu=44\,\mathrm{g/mol} , the initial volume is V1=0.03m3,V_1=0.03\,\mathrm{m}^3, the initial pressure is p1=1.025bar=1.025105Pap_1 = 1.025\,\mathrm{bar} = 1.025\cdot10^5\,\mathrm{Pa} . The final pressure is p2=6.15bar=6.15105Pa.p_2= 6.15\,\mathrm{bar}=6.15\cdot10^5\,\mathrm{Pa}.


(i) If pV1.4=constant,pV^{1.4}=\text{constant}, then p1V11.4=p2V21.4    V2=V1(p1p2)1/1.4=8.3103m3.p_1V_1^{1.4} = p_2V_2^{1.4} \; \Rightarrow \; V_2 = V_1\left( \dfrac{p_1}{p_2}\right)^{1/1.4} = 8.3\cdot10^{-3}\,\mathrm{m^3}. For such a polytropic process the work can be calculated as

A=pdV=νR1.41T1(1T2T1)A = \int p\,dV =\nu \dfrac{R}{1.4-1}\cdot T_1\left( 1-\dfrac{T_2}{T_1}\right) .

p1V1=mμRT1,  T1=325.6K;    p2V2=mμRT2,  T2=540.5K.p_1V_1 = \dfrac{m}{\mu}RT_1, \; T_1 = 325.6\,\mathrm{K} ; \;\; p_2V_2 = \dfrac{m}{\mu}RT_2, \; T_2 = 540.5\,\mathrm{K}.

Therefore, the work of gas will be A=νR1.41T1(1T2T1)=5073J.A =\nu \dfrac{R}{1.4-1}\cdot T_1\left( 1-\dfrac{T_2}{T_1}\right) = -5073\,\mathrm{J}.

The heat that should be given to gas can be calculated as

q=Tds=νcv1.41.31.41(T2T1)=3Rν1.41.31.41(540.5325.6)=1522J.q=\int T\,ds =\nu c_v \dfrac{1.4-1.3}{1.4-1}(T_2-T_1) = 3R\cdot \nu\cdot \dfrac{1.4-1.3}{1.4-1}(540.5-325.6) = 1522\,\mathrm{J}.


(ii) In the isothermal process T1=T2=325.6K.T_1=T_2 = 325.6\,\mathrm{K}. For such process work can be calculated as

A=pdV=νRTlnV2V1=νRTlnp1p2=5509J.A = \int p\,dV =\nu R T\ln \dfrac{V_2}{V_1} = \nu R T\ln \dfrac{p_1}{p_2} = -5509\,\mathrm{J}. The change of internal energy is 0, so the heat that should be given to the gas is 5509J.-5509\mathrm{J}.


(iii) if the cylinder is thermally insulated the heat flow will be 0, so the process will be adiabatic. Let us calculate the final temperature:

pV1.3=constant,    p1V11.3=p2V21.3    V2=V1(p1p2)1/1.3=7.56103m3.pV^{1.3}=\text{constant}, \;\; p_1V_1^{1.3} = p_2V_2^{1.3} \; \Rightarrow \; V_2 = V_1\left( \dfrac{p_1}{p_2}\right)^{1/1.3} = 7.56\cdot10^{-3}\,\mathrm{m^3}.

p2V2=mμRT2,  T2=492.4K.p_2V_2 = \dfrac{m}{\mu}RT_2, \; T_2 = 492.4\,\mathrm{K}.

The work of the gas is equal to A=(U2U1)=cvν(T1T2)=3Rν(T1T2)=4725J.A = - (U_2-U_1) = c_v\nu (T_1-T_2) = 3R\nu (T_1-T_2) = -4725\,\mathrm{J}.


We may notice that the work of the gas is negative, so we should do work on gas

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