1.109 Air enters the converging nozzle shown in Fig. P1.72 at \(T_{1}=70^{\circ} \mathrm{F}\) ard \(V_{1}=50 \mathrm{ft} / \mathrm{s} .\) At the exit of the nozzle, \(V_{2}\) is given by \\[ V_{2}=\sqrt{V_{1}^{2}+2 c_{p}\left(T_{1}-T_{2}\right)} \\] where \(c_{p}=187 \mathrm{ft} \cdot \mathrm{lb} / \mathrm{lbm} \cdot^{\circ} \mathrm{F}\) and \(T_{2}\) is the air temperature at the exit of the nozzle, Find the temperature \(T_{2}\) for which \(V_{2}=\) \\[ 1000 \mathrm{ftfs} \\]

Short Answer

Expert verified
Calculate the resulting expression for \(T_{2}\). This returns the air temperature at the exit of the nozzle given that the air exit velocity is \(1000 \mathrm{ft} /\mathrm{s}\).

Step by step solution

01

Rearrange the Equation for \(T_2\)

We first need to rearrange the equation \(V_{2} = \sqrt{V_{1}^{2} + 2c_{p}(T_{1} - T_{2})}\) to isolate \(T_2\) on one side of the equation. Squaring both sides, and then solving for \(T_2\), we get \[T_{2} = T_{1} - \frac{{V_{2}^{2} - V_{1}^{2}}}{{2c_{p}}}\] This allows us to insert the given or known values into the equation.
02

Insert Known Values Into the Equation

We're given \(T_{1} = 70^{\circ} \mathrm{F}\), \(c_{p} = 187 \mathrm{ft} \cdot \mathrm{lb} / \mathrm{lbm} \cdot^{\circ} \mathrm{F}\), \(V_{1} = 50 \mathrm{ft} / \mathrm{s}\) and \(V_{2} = 1000 \mathrm{ft} / \mathrm{s}\). We substitute these given values into the equation.\[T_{2} = 70^{\circ} \mathrm{F} - \frac{{(1000 \mathrm{ft} / \mathrm{s})^{2} - (50 \mathrm{ft} / \mathrm{s})^{2}}}{{2 \times 187 \mathrm{ft} \cdot \mathrm{lb} / \mathrm{lbm} \cdot^{\circ} \mathrm{F}}}\]
03

Evaluate the Expression for \(T_2\)

Next we perform the mathematical operations to solve for \(T_{2}\). This gives us the final temperature at the nozzle exit. Only one answer will be produced by these calculations.

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