The static pressure to stagnation pressure ratio at a
Chapter 11, Problem 11.36(choose chapter or problem)
The static pressure to stagnation pressure ratio at a point in a gas flow field is measured with a Pitot-static probe as being equal to 0.6. The stagnation temperature of the gas is \(\mathrm{20 ~^\circ C}\). Determine the flow speed in m/s and the Mach number if the gas is air. What error would be associated with assuming that the flow is incompressible?
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