Q$1-)$ Air is released steadily from a reservoir and delivered to the nozzle with a diameter of $d=0\mathrm{.}01$ by the pipe with a diameter of $D=0\mathrm{.}03m$ to blow the air into the atmosphere as shown in Figure $1.$ Determine the volume flow rate and static $($gage$)$ pressure in the pipe at point $2,$ assuming the pressure in the tank remains constant at $3\mathrm{.}0$ kPa. Please note that the density of the air in the tank is obtained from the perfect gas law, using standard absolute pressure and temperature $($Air temperature in the reservoir is $15C).$ The gas constant of air is $R=0\mathrm{.}287$kPa$*\frac{m^3}{k}g*K$