Question
The air velocity in the duct in Fig. $P 11.12$ is $750 \mathrm{ft} / \mathrm{s}$. The air static temperature is $100^{\circ} \mathrm{F}$. Use the mercury manometer measurement to calculate the static and stagnation pressures of the flowing air.
Step 1
The conversion formula is $T_{R} = T_{F} + 459.67$. So, $T = 100^{\circ}F = 100 + 459.67 = 559.67 R$. Show more…
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