A pilot attempts to pull up a maneuver $(5$ km above the sea level$)$ at an angle of $30$ degree $($see Figure$).$

If the supplied heat energy is $4\mathrm{.}5k\frac{j}{k}g$ and the diameter of the inlet is $2\mathrm{.}5$ m $,$ estimate the power output

from one of its Pratt and Whitney compressor $(70\%$ efficiency$).[$Use literature reviews from chapter $(1)$ to

$(4)].$ Assume standard atmospherics conditions at sea level.