Respuesta :
Answer:
a) The exit temperature is 39.25°C
b) The highest component surface is 132.22°C
c) The average temperature for air equal to 35°C is a good assumption because the air temperature at the inlet will increase due to the result in the heat gain produced by the duct and whose surface is exposed to a flow of hot.
Explanation:
a) The properties of the air at 35°C:
p = density = 1.145 kg/m³
v = 1.655x10⁻⁵m²/s
k = 0.02625 W/m°C
Pr = 0.7268
cp = 1007 J/kg°C
a) The mass flow rate of air is equal to:
[tex]m=\rho *V = 1.145*0.65=0.7443kg/min=0.0124kg/s[/tex]
The exit temperature is:
[tex]T=T_{i} +\frac{Q}{m*c_{p} } =27+\frac{0.85*180}{0.0124*1007} =39.25[/tex]°C
b) The mean fluid velocity is:
[tex]V_{m} =\frac{V}{A} =\frac{0.65}{0.16*0.16} =25.4m/min=0.4232m/s[/tex]
The hydraulic diameter is:
[tex]D_{h} =\frac{4A}{p} =\frac{4*0.16*0.16}{4*0.16} =0.16m[/tex]
The Reynold´s number is:
[tex]Re=\frac{VD_{h} }{v} =\frac{0.4232*0.16}{1.655x10^{-5} } =4091.36[/tex]
Assuming fully developed turbulent flow, the Nusselt number is:
[tex]Nu=0.023Re^{0.8} *Pr^{0.4} =0.023*4091.36^{0.8} *0.7268^{0.4} =15.69[/tex]
[tex]h=\frac{k*Nu}{D_{h} } =\frac{0.02625*15.69}{0.16} =2.57W/m^{2} C[/tex]
The highest component surface temperature is:
[tex]T=T_{e} +\frac{\frac{Q}{A} }{h} =39.2+\frac{0.85*\frac{180}{4*0.16*1} }{2.57} =132.22[/tex]°C