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The velocity of an air stream is 20 m/s. The densities of mercury and air are 13600 kg/m3 and 1.2 kg/m3, respectively. The gravitational acceleration may be taken as 10 m/s2. When a Pitot-static tube is placed in the stream, assuming the flow to be incompressible and frictionless, the difference between the stagnation and static pressure in the flow field (in mm Hg) would approximately be

  • A.1760
  • B.1.76
  • C.0.57
  • D.\(0.57 \times 10^{-5}\)

Answer: B

The pressure difference is about 1.76 mm Hg.

A Pitot-static tube reads the dynamic pressure, the difference between stagnation and static pressure:

\[ \begin{aligned} \Delta p &= \tfrac{1}{2}\rho_{air}V^{2} = \tfrac{1}{2}(1.2)(20)^{2} = 240\ \text{Pa} \\ h &= \frac{\Delta p}{\rho_{Hg}g} = \frac{240}{13600 \times 10} \\ &= 1.76 \times 10^{-3}\ \text{m} = 1.76\ \text{mm} \end{aligned} \]

1760 is the same column expressed in micrometres, a units slip. 0.57 is the reciprocal of 1.76, and \(0.57 \times 10^{-5}\) compounds that with a wrong power of ten.

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