Thermodynamics: An Engineering Approach 8th Edition

Published by McGraw-Hill Education
ISBN 10: 0-07339-817-9
ISBN 13: 978-0-07339-817-4

Chapter 13 - Gas Mixtures - Problems - Page 717: 13-39

Answer

$\dot{m}=6.65\ \text{kg/min}$

Work Step by Step

The molar fraction of air is $$ y_{\text {air }}=1-y_{\mathrm{CH} 4}=1-0.15=0.85 $$ The molar mass of the mixture is determined from $$ \begin{aligned} M_m & =y_{\mathrm{CH} 4} M_{\mathrm{CH} 4}+y_{\text {air }} M_{\text {air }} \\ & =0.15 \times 16+0.85 \times 28.97 \\ & =27.02 \mathrm{~kg} / \mathrm{kmol} \end{aligned} $$ Given the engine displacement and speed and assuming that this is a 4-stroke engine flow rate is determined from ($2$ revolutions per cycle), the volume flow rate is determined from $$ \dot{V}=\frac{\dot{n} V_d}{2}=\frac{(3000 \mathrm{rev} / \mathrm{min})\left(0.005 \mathrm{~m}^3\right)}{2 \mathrm{rev} / \mathrm{cycle}}=7.5 \mathrm{~m}^3 / \mathrm{min} $$ The specific volume of the mixture is $$ v=\frac{R_u T}{M_m P}=\frac{\left(8.314 \mathrm{kPa} \cdot \mathrm{m}^3 / \mathrm{kmol} \cdot \mathrm{K}\right)(293 \mathrm{~K})}{(27.02 \mathrm{~kg} / \mathrm{kmol})(80 \mathrm{kPa})}=1.127 \mathrm{~m}^3 / \mathrm{kg} $$ Hence the mass flow rate is $$ \dot{m}=\frac{\dot{v}}{v}=\frac{7.5 \mathrm{~m}^3 / \mathrm{min}}{1.127 \mathrm{~m}^3 / \mathrm{kg}}=6.65 \mathrm{~kg} / \mathrm{min} $$
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