Problem $04\mathrm{.}023-$ Determine pressure measurement by a Pitot tube

A Pitot tube is mounted in the test section of a high$-$speed subsonic wind tunnel. The pressure and temperature of the airflow are $1$ atm

and $258$ K $,$ respectively. If the flow velocity is $262\frac{m}{s},$ what is the pressure measured by the Pitot tube?

The pressure measured by the Pitot tube is

${10}^5\frac{N}{m^2}$