The stators in a gas turbine are designed to increase the kinetic energy of the gas passing through them adiabatically. Air enters a set of these nozzles at 300 psia and 700°F with a velocity of 82 ft/s and exits at 250 psia and 645°F. Calculate the velocity at the exit of the nozzles. The specific heat of air at the average temperature of 672.5°F is cp = 0.253 Btu/lbm·R.

Respuesta :

Given Information:

Inlet Temperature = T₁ = 700° F

Exit Temperature = T₂ = 645° F

Inlet Velocity = v₁ = 82 ft/s

Specific heat of air = cp = 0.253 Btu/lbm.R

Required Information:

Exit velocity = v₂ = ?

Answer:

Exit velocity = [tex]v_{2}= 838.75[/tex]  [tex]ft/s[/tex]

Explanation:

As we know the energy balance equation is given by

[tex]E_{in} = E_{out}[/tex]

[tex]m(h_{1} + \frac{v_{1}^2 }{2}) = Q_{out} + m(h_{2} + \frac{v_{2}^2 }{2})[/tex]

[tex](h_{1} + \frac{v_{1}^2 }{2}) = (h_{2} + \frac{v_{2}^2 }{2})[/tex]

[tex]v_{2}^2= v_{1} ^2 +2(h_{1} - h_{2} )[/tex]

[tex]v_{2}= \sqrt{ v_{1} ^2 +2(h_{1} - h_{2} )}[/tex]

[tex]v_{2}= \sqrt{ v_{1} ^2 +2c_{p} (T_{1} - T_{2} )}[/tex]

1 Btu/lbm is equal to 25037 ft²/s²

[tex]v_{2}= \sqrt{ (82 ft/s)^2 +2*0.253\frac{Btu}{lbm.R} (700 - 645)R *25037\frac{\frac{ft^2}{s^2}}{1\frac{Btu}{lbm}} }[/tex]

[tex]v_{2}= 838.75[/tex]  [tex]ft/s[/tex]