Question 2.8: A mixture of CO and air is 10% fuel rich by volume and at 8....

A mixture of CO and air is 10% fuel rich by volume and at 8.28 bar and 555K. The mixture burns adiabatically and at constant volume. Calculate the products temperature neglecting dissociation.

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The representative stoichiometric reaction equation gives the ideal reaction, which shows the required oxygen and nitrogen to thoroughly combust all the fuel:

CO + \frac{1}{2}O_{2} + \frac{1}{2} \times 3.76N_{2} \rightarrow CO_{2} + \frac{1}{2} \times 3.76N_{2}

We know that the reaction is not stoichiometric, because we are told that the mixture is 10% rich – i.e. there is 10% more CO than can be burnt with the stoichiometric air in the above equation. Therefore, the true representative reaction equation will have 1.1CO, thus:

1.1CO + \frac{1}{2}O_{2} + \frac{1}{2} \times 3.76N_{2} \rightarrow CO_{2} + \frac{1}{2} \times 3.76N_{2} + 0.1CO

Alternatively, divide by 1.1 to get the reaction in terms of combustion of 1 kmol of fuel:

CO + 0.91(\frac{1}{2}O_{2} + \frac{1}{2} \times 3.76N_{2} ) \rightarrow 0.9CO_{2} + 1.71N_{2} + 0.0CO

In order to determine the final temperature, we need to analyse the closed system with the method described above:

U_{2}  –  U_{1} = \sum\limits_{PRODUCTS}{m_{i}cv_{i}}(T_{2}  –  T_1)    – \sum\limits_{PRODUCTS}{m_{i}cv_{i}}(T_{2}  –  T_1) +\Delta U_{0}

The internal energy of combustion can be obtained from the tabulated values of enthalpy of combustion and the equation to convert between the two:

\Delta H_{0} = \Delta U_{0} + \Delta  (n_{p}  –  n_{R}) RT_{0}

\Delta \tilde{h_{0}} for CO is –283 000 kJ/kmol for the reaction CO + \frac{1}{2}O_{2} \rightarrow CO_{2}

\Delta \tilde{u}_{0} = \Delta \tilde{h}_{0} – (n_{p} – n_{R}) \tilde{R}T

 

\Delta \tilde{u}_{0} = -283 000 – (1 – 1.5)8.314 \times 298

Therefore the internal energy of combustion per kmol of CO is – 281 761 kJ/kmol.
To put this in specific terms, divide by the molecular mass of CO, 28 kg/kmol, to give –10 063 kJ/kg.
The first law can now be applied, for adiabatic (Q = 0) and constant volume (W = 0) to give:
                                       U_{2}  –  U_{1} = 0

Where U_{2}  is the total internal energy of the products at the end of the process and U_{1} is the total internal energy of the reactants before combustion. Knowing the temperature of the reactants, we can work out the internal energy of the reactants before combustion.
We don’t know the final temperature of the products – this is what is asked for. Using equation (2.44):

U_{2}  –  U_{1} = \sum\limits_{PRODUCTS}{m_{i}cv_{i}}(T_{2}  –  T_1)   – \sum\limits_{PRODUCTS}{m_{i}cv_{i}}(T_{2}  –  T_1) +\Delta U_{0}

And reading values of molar internal energy from the tables (Rogers and Mayhew, 1995), to complete the following table of reactants:

Species n_{i}   kmol \tilde{u}_{i,555K} kJ/kmol n_{i}\tilde{u}_{i,555K} kJ/kmol
CO 1 2984 2984
O_{2} 0.455 3233 1471
N_{2} 1.71 2944 5034
Σ 9489

where the internal energy at 555K is found from the tables by interpolation. Values are stated at 400K and 600K for a number of gaseous species. The interpolation is done thus:

\tilde{u}_{i,555K} = \frac{555  –  400}{600  –  400}(\tilde{u}_{i,600K}  –  \tilde{u}_{i,400K}) + \tilde{u}_{i,400K}

The reader can easily confirm that the values in the table are correct.
There is no direct way to obtain the product temperature since it is determined by balancing the equation. The method used is to guess a temperature and see how far out  of balance the equation is. In this case, guess 3000K.
Making the same table as above for the products

Species n_{i}   kmol \tilde{u}_{i,3000K} kJ/kmol n_{i}\tilde{u}_{i,3000K} kJ/kmol
O_{2} 0.91 127 920 116 407
CO 0.09 68 598 6174
N_{2} 1.71 67 795 115 929
Σ 238510

Inserting the values in the equation:

U_{2}  –  U_{1} = 238 510  –  9489  +  (–281 761) = –52 740 kJ

This is negative, and shows that the products were not hot enough. Therefore try the next temperature up in the table, i.e. 3200K:

Species n_{i}   kmol \tilde{u}_{i,3200K} kJ/kmol n_{i}\tilde{u}_{i,3200K} kJ/kmol
O_{2} 0.91 138 720 126 235
CO 0.09 74 391 6695
N_{2} 1.71 73 555 125 779
Σ 258 709

And the equation now is

U_{2}  –  U_{1} = 258 709  –  9489 + (-281 761) = –  32 540  kJ

This is still too cool so the process is repeated until the answer is acceptably close to  zero.

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